SMART Rotor Wind Tunnel Test Report

Appendix A—SMART Rotor Test Runs, Wind Tunnel and Whirl Tower

Smart Rotor Test Runs -- Wind Tunnel Run Run Date Objective Objective, Comments Active Data Run Time, hr: min BA NFAC Control Record Proce Rotor Amplifier Tunnel -- 21-Feb attempted transmission run aborted due to MG set problem FltTape Drive 1 -- 2/22 initial transmission run checkout motor control or AFC 0 -- -- 2/26 amplifier test, using RC loads hand recorded data -- -- 2/28-3/1 Motor run, etc. preliminary runs 48448 0 2 -- 3/3 hydraulic accumulator test 5Gal = 1800psi; 10Gal = 270psi 3 -- 3/4 hub run, balance, up to 110%NR exercise mixed and direct controls 48408 1 4 -- 3/10 hydraulic accumulator test 5Gal = 1000psi; 10Gal = 270psi 5 -- 3/10 rotor balance and static mast check loads hand recorded data 6 -- 3/13 hub weight tare (doors open) checkout alpha control 48409 1 7 -- 3/13 rotation tare, aborted at motor start (doors open) due to incomplete 80x to 40x conversion 8 6 3/14 rotation tare (doors open) w acoustic traverse 48410 1 9 6 3/14 aero tare set, test overspeed at 107%, 420Rpm 48410,11 1 ?

10 -- 3/18 rotor check loading hand recorded data 11 11,12 3/19 blade weight tare, rotor track and balance, stability controls sweep, accumulator test 48412 1 2:24 12 -- 3/20 rotor track and balance, stability up to 105%NR track with strobe 48413 1 0:31 13 16 3/24 rotor track and balance, controls sweep track with strobe 48414 1 1:42 14 21 3/26 forward flight checkout - 41, 62 knots limited by fbm torsion, tunnel/motor interlock off test 48415 1 2:09 ?

15 22 3/26 Forward flight checkout, 82, 103, 124 knots fbm torsion loads 48416 1 2:45 ?

16 -- 3/27 actuator and amplifier checkout non-rotating AFC 1 17 24 3/28 Open loop checkout, hover, 42, 62kt Sine mode only (not synched to azimuth) 48417 1 2:14 ?

freq sweeps in hover 18 -- 3/29 rotor check loading 48418 1 19 -- 4/1 closed loop control checkout non-rotating (HHC) 48419 1 20 27 4/2 open, closed loop checkout, 82, 124 kts Alfa, CT sweep at 82kt, fan brg temp (HHC) 48420 1 2:30 2:23 21 28 4/3 run stopped after checkout of tare reduction implemented tare correction 48421 0 0:32 22 29 4/3 run stopped after checkout of flap control implemented software correction 48421 1 23 31 4/7 open, closed loop DARPA points, 123kt alfa, CT sweep 124kt, instrumentation problem (HHC) 48422 1 3:06 0:25 tunnel E-stop initiated 24 32 4/8 open, closed loop DARPA points, 123kt (HHC) 48423 1 1:51 1:38 25 34 4/9 open loop DARPA points, 83, 155kt alfa, CT sweep at 154kt; pitchcase loads (HHC) 48425 1 1:42 1:29 tunnel E-stop, unknown reason, fly down 26 35 4/10 open, closed loop DARPA points, 123kt; BDM frequency, 4P phase sweeps at 124kt (HHC) 48425 1 2:30 2:19 27 -- 4/10 attempted run tunnel not starting y 0 28 38,39 4/11 frequency sweep in hover 200V, 0.2-80Hz 48426 1 3:00 2:34 freq sweep, 5,6,3,2P phase sweeps at 124kt alfa sweep at 82kt for max BVI at 0V 29 41 4/14 200V freq sweeps (0-80, .2-9) col,lon,lat 82kt alfa sweep at 62,103kt for max BVI at 0V 48428 1 2:25 2:12 250V 4P virt sp lat phase sweep at 82kt alfa, CT sweep at 82kt 30 42 4/15 DARPA4 at 83kt, alfa=0.89; w pos cntl 250V 4,5,6,3,2P phase sweeps.; CTC CTC 48429 1 2:51 2:40 DARPA2,1 at 123kt, alfa=-9.4; w pos cntl 31 44 4/16 combined ampl, phase sweps at 82kt, alfa=2 ---> 250-500V 2P90, 1.5deg 2P90 90+/-15 Mic1 CTC (48430) 1 2:29 2:23 traverse 0deg, 1.5deg 2P90 at 82kt, alfa=2 250-450V 3P240, 1.5deg 3P240+/-15 Mic13 200V freq sweep (0-80) col,lon,lat at 124kt,alfa=-9.1 150-300V 4P90, 1.5deg 4P90+/-15 Mic1 150-350 5P0, 1.5deg 5P0+/-15 Mic1 32 45 4/17 closed loop vib cntl at 82kt alfa=2 200V 0-80Hz sweep col CTC AFC 1 2:43 2:32 NF 5,1,1-5P; RM 5,1-5P w col; CTC 1.5deg 2P phase sweep; 1.5-3deg 2P300,90,105 Mic1 at 82kt, alfa=2 33 46 4/18 closed loop vib cntl at 124kt, alfa=-9.1 175/200V 0-80Hz col,lon,lat; Mic13 transfer fctn CTC 48431 1 2:56 2:36 NF 1-5P, PM 1-5P, Mic1 5,1-5P 1.5deg 3P phase sweep, 1.5-2deg 3P230-250, Mic13 at 124kt, alfa=-9.1 1.5deg 5P phase sweep, 1-2deg 5P70-100, Mic13 at 124kt, alfa=-9.1 control power at 124kt, alfa=-9.1; lon, lat closed loop noise cntl at 124kt, alfa=-9.1, Mic16 5, 1-5P DARPA2,1 at 123kt, alfa=-9.4; w pos cntl CTC 34 48 4/22 control power at 82kt, alfa=-5.5 and 2 200V 0.2-9Hz col, lon,lat HHC 48432 1 2:27 2:15 swashplate, flap virtual s/p and IBC inputs, HHC 35 49 4/22 1.5deg 3,4,5,2P phase sweeps at 82kt alfa=2 amplitude sweeps at optimal freq. and phase, CT CTC 48433 1 2:14 1:55 microphone traverse, baseline and optimal open loop; 1.5deg 3P180 36 52 4/23 1.5deg 3,4,5,2P phase sweeps at 62kt alfa=4 amplitude sweeps at optimal freq. and phase CTC 48434 1 2:52 2:40 microphone traverse, baseline and optimal open loop; 1.5deg 4P30 37 53,54 4/24 control power at 124kt, alfa=-9.1 150V col, 200V lon, 175V lat 0.2-9Hz; HHC HHC 48435 1 2:50 2:43 swashplate, flap virtual s/p and IBC inputs; inplane noise, mic13 at 124kt, -9.1deg 1.0deg 4P, 1.5deg 2P phase sweeps; CTC CTC 3P+5P combined optimal open loop (SH) 38 55 4/24 inplane noise, mic13 at 124kt, -9.1deg amplitude sweeps at optimal freq. and phase CTC 48436 1 2:10 1:56 1deg 3P250 +1deg 2P phase sweep 1deg 3P250 +1/.75/.5deg 4P phase sweep rotor smoothing, 124kt, -9.1deg flap1 +3/-3deg, flap2 +3/-3deg, w 1deg increment performance, 124kt, -9.1deg CT/S=.04-.09, w 0deg and 0V, no retrim 39 57 4/25 Rotor smoothing, hover flap1 +3/-3deg, flap2 +3/-3deg, w 1deg increment CTC 48437 1 2:59 2:43 inplane noise, mic13 at 124kt, -9.1deg Inplane 3P+2P, 3P+4P amplitude variations Vibration closed loop control CTC2 at124kt, -9.1deg NF 1-5P, PM 1-5P, T=10,1 Performance, open loop 2P phase sweep at 124kt, - CT/S=0.075 traverse sweep at 103kt, -4deg microphone traverse, baseline

Appendix A—SMART Rotor Test Runs, Wind Tunnel and Whirl Tower (cont.)

Smart Rotor Test Runs -- Wind Tunnel Run Run Date Objective Objective, Comments Active Data Run Time, hr:min BA NFAC Control Record Proce Rotor A mplifier Tunnel 40 58 4/26 Vibration closed loop control HHC 62, 68kt NF 5Pat 62kt, NF,RM,PM 5P at 68kt HHC 48438 1 2:17 2:08 BVI noise, mic9 at 62kt, 4deg 2P-5P combined optimal open loop (SH) BVI noise, mic9 at 68kt, 1.8deg phase, ampl. sweep, open loop microphone traverse, baseline and optimal open loop; 1.5deg 3P180 41 59,61 4/26 Vibration closed loop control at 82kt, 2deg HHC NF, RM,3F, NF,RM,PM HHC 48439 1 2:28 2:17 BVI open loop optimal control at 82kt, 2deg 2P-5P combined optimal open loop (SH) performance, 82kt, 2deg CT/S=.04-.10, w 0deg and 0V, no retrim Rotor smoothing 82kt, 2deg flap1 +3/-3deg, w 1deg increment DARPA4 at 83kt, HHC vs CTC HHC, CTC 42 63 4/28 Rotor dynamics in hover frequency sweeps col,lon,lat at 2deg collective CTC 48440 1 2:14 2:01 Vibration closed loop control CTC3 at 124kt NF 10P, T=5,1; NF 1-5,10P, T=10,5 Inplane open loop optimal control at 124kt 2P-5P combined optimal open loop (SH) Performance, open loop 2P phase sweep at 124kt CT/S=0.090 DARPA3 at 155kt 0deg data 43 64 4/28 BVI noise, Mic1 closed loop control at 62kt, 4deg Mic1 4P, 2-5P, RMS, 10-50N HHC 48441 1 2:23 2:06 BVI noise, Mic1 closed loop control at 82kt, 2deg Mic1 4P, 2-5P, RMS, 10-50N BVI noise, Mic13 closed loop control, 124kt, -9.1deg Mic13 4P, 2-5P, RMS,1-6N Vibration closed loop control at 124kt NF 5,1-5P, RM 5,1-5P Actuator baseline performance 200-400V 1Hz; 75V, 0-200Hz col,lin 44 -- 4/29 Actuator baseline performance, amplifier check 200-400V 1Hz; 75V, 0-200Hz AFC 1 45 -- 4/29 blade weight tare (repeat of 3/19) w hydraulics on 48449 1 46 -- 4/29 Amplifier check, power sharing 400 +/-600V, 6,12,18P AFC 1 47 -- 4/29 Checkloads, blade, balance 48449 1 Total 39 65.2 hrs 45.9 Smart Rotor Test Runs -- Whirl Tower 1 11/26 initial motor/transmission run Whirl Tower 2007 2 12/6 accumulator test 3 1/24 initial hub run Whirl Tower 2008 48442 4 1/25 hub run, exercise controls 48443 5 2/1 rotor track and balance, stability testing, controls sweep, up to 107%NR 48444 1:16 6 2/1 rotor track and balance 48444 0:35 7 2/5 track and balance, open loop flap control 48445 1:22 8 2/6 track and balance, open loop flap control, frequency sweeps 48446 1:08 9 2/7 track and balance, open loop flap control, frequency sweeps 48447 0:46 Total 5.1 hrs Notes HHC - higher harmonic control, position control of 0-5P; (HHC) - checkout, results not reliable.

CTC - continuous time HHC, position control of 0-6p.

AFC - data not recorder on tape; only PC-based data available.

Pre and post test checkout test runs are: 2,4,5,10,16,18,19, 44,45,46,47.

Runs 9-13: Boeing and NFAC point numbers not correlated.

Run 15: started using auto setup to generate ASAP labels..

Run 20+: Microphone cal/gain data entered for correct Boeing point numbers, correct starting Run 20.

Run 28: FA1CmdVoltage is now up; actually is command for flap 2.

Run 31: lost IRIG time, lost Heim recorder, apparent loss of some rot. instrumentation during Pt 127, ok after RPCM reboot.

MUX tape damaged, continued w/o Heim recorder, AFC time code may not be usable; fixed October 2008.

Tape 48430 could no longer be read in 2009. Data acquired from tape in 2008 with gaps filled is used.

Runs 31,32,33: NFAC 11sec off; add +11-2s; provide 14s of time slice; fixed October 2008.

Run 32: was not recorded on tape.

Run 39: CTC controller unstable after Pt 56.

Flight test tape 48427 does not exist.

Appendix B—SMART Rotor 40x80 Test – Tare Data Curve Fits, 2008

1.1 SUMMARY This document lists the various tare data curve fits used during the test of the SMART Rotor at the NFAC 40x80 wind tunnel in March–April, 2008.

1.2 BACKGROUND The basic procedure for using tare data is described in the Software Plan. The tare data was extracted from the following test runs.

Test # Description 6 Weight tare with hub only, shaft angle varied 8 Rotation tare with hub only, shaft angle varied 9 Aero tare with hub only, shaft angle and tunnel speed varied 11 Weight tare with hub and blades, shaft angle varied The statistical data from the above tests were provided to NFAC for deriving the tare curve fits. The resulting polynomial curve fits for the weight and rotation tares were taken from results provided by Benton Lau. The polynomial coefficients for the aero tare were taken from results provided by Randy Peterson.

In the post-run data processing, no tare allowances up to and including test 6. Hub weight tare data allowance is made for test 8, while hub weight and shaft rotation tare allowances are made for test 9. Starting with test 11 (the first blades-on run), all of the tare curve fits are used.

It was also assumed that zeros would be taken for the balance loads and torque so that the various tare polynomial curve fits would not have a constant term in them.

1.3 HUB WEIGHT TARE The hub weight tare polynomials are of the following form.

Correction = c α + c α

2 s u 1 s u As noted above, there is no constant term independent of the shaft angle as a result of the fact that zeros are taken for the balance loads and torque.

Quantity c2 c1 Axial 0 1.65593844E+01 Side 0 0 Normal 1.50628879E-01 6.11545805E-03 Roll 0 0 Pitch 0 3.47832811E+02 Torque 0 0 1.4 SHAFT ROTATION TARE The polynomial form is the same as that used above for the hub weight tare.

Quantity c2 c1 Axial 0 1.51569176E+01 Side 0 0 Normal 1.96238481E-01 8.03048333E-01 Roll 0 0 Pitch 0 3.49176260E+02 Torque 0 0 1.5 BLADE WEIGHT TARE The polynomial form here is also of the same form as for the hub weight tare.

Quantity c2 c1 Axial 0 2.07534609E+01 Side 0 0 Normal 1.95654729E-01 -9.16578705E-02 Roll 0 0 Pitch 0 4.12665804E+02 Torque 0 0 1.6 AERO TARE Due to the nature of the data, the aero tares were calculated in two tunnel speed ranges, one set for tunnel dynamic pressure up to 40 lb/ft and a different set for tunnel dynamic pressure above this range. The compound polynomial that was fitted to the tare data is of the following form.

2 2

Correction = ( c + c α + c α ) + ( d q + d q )

0 1 2 1 2 su su The coefficients for dynamic pressure less than 40 lb/ft are given below.

Quantity c0 c1 c2 d1 d2 Axial 4.41635E+01 3.5469E-01 -9.6949E-03 5.3657E+00 -6.87172E-02 Side -2.60047E+01 -5.3582E-01 1.73582E-02 1.85598E+00 -4.32008E-02 Normal -3.32883E+01 4.05031E+00 -1.50037E-01 -1.59653E+00 3.87342E-02 Roll 9.12508E+01 -3.75755E+01 1.12821E+00 -3.53552E+01 6.87260E-01 Pitch 2.93151E+02 1.64353E+01 -3.96708E-01 1.71517E+02 -7.36995E-01 Torque 1.40081E+03 -3.64107E+00 -7.98055E-02 2.45818E+01 -1.12240E-01 The coefficients for dynamic pressure greater than 40 lb/ft are shown in the following table.

Quantity c0 c1 c2 d1 d2 Axial -9.21234E+02 -1.22059E+00 -5.54287E-02 3.32231E+01 -2.23995E-01 Side 5.39620E+02 -1.29505E+00 -4.94794E-02 -1.74372E+01 1.28125E-01 Normal 3.04635E+03 1.44131E+01 -3.01163E-01 -9.66043E+01 7.21733E-01 Roll 3.51931E+03 -1.19794E+02 -1.30131E-01 -1.31035E+02 9.48338E-01 Pitch 4.27314E+03 3.49026E+01 -3.56435E+00 3.04429E+01 7.91147E-01 Torque -4.21734E+03 -1.65780E+01 -5.23099E-01 2.01120E+02 -1.40240E+00 In all of the above curve fits, the uncorrected shaft angle is in degrees and the uncorrected tunnel dynamic pressure is in lb/ft .

Appendix C—Checklist

SMART Rotor Pre-Run Checklist, V3.1

Test No. Boeing, NFAC

Date

Time

Inspections:

Rotor head assy

Rotor blade/flap assy

Control system

Hydraulics

Motor/test stand

Model/Instrumentation Changes:

Test stand/model

Instrumentation/software

Flap actuator control/software

Control Room/Data Computer:

Deg F

% RH

Hydraulic cart on, verify pressure

Motor cooling water (chiller) on

Amplifier on, two fans on

Instrumentation up & recording

Strip charts: up & recording

Rotor control mode normal

Unlock controls

Set rotor controls to ten collective, zero cyclic

Take pre-run zero, Rcal

Switch amplifier relays on, set Vbias to 400

Set rotor controls to zero collective, zero cyclic

Take pre-run zero

Set controls to collective required for start up

Scavenge pump on

Mister on (30–45 drops/min)

Health monitor up & recording

SMART Rotor Post-Run Checklist

Normal Shutdown Procedure:

Set controls to collective required for shutdown, zero cyclic

Command rotor speed to zero

Set controls to zero collective, zero cyclic

Take post-test zero

Set controls to ten collective, zero cyclic

Switch amplifier relays off, set Vbias to 0

Take post-test zero, Rcal

Control Room Shutdown:

Lock rotor controls

Mister off

Scavenge pump off

Amplifiers off; stop fans 10 min later

Instrumentation, HMS, strip charts off

Engineering & HMS data saved and archived

7.0 0.075 0.075 0.040 0.040 0.075 0.075 0.075 0.075 0.090 [CT/s] 0.075 0.075 0.075 0.075 0.075 0.040 Col (deg) 0.04, 0.045 0.06, 0.075 0.040, 0.060, 0.075 0.040, 0.060, 0.065 0.040, 0.060, 0.070 0.040, 0.060, 0.070 0.040, 0.060, 0.070 0.040, 0.060, 0.070 0.060, 0.075 0.080, 0.090 0.040, 0.060, 0.075, 0.080 0.040, 0.060, 0.075 0.080, 0.090 0.040, 0.060, 0.075, 0.080, 0.090 0.040, 0.060, 0.075, 0.080, 0.090 0.040, 0.060, 0.075, 0.080, 0.090 0.040, 0.060, 0.075, 0.080, 0.090 0.050, 0.060, 0.075, 0.080, 0.090 0.040, 0.060, 0.075, 0.080, 0.090 0.040, 0.060, 0.075, 0.080, 0.090, 0.100 0.040, 0.060, 0.075, 0.080, 0.090, 0.100 0.040, 0.060, 0.075, 0.080, 0.090, 0.100 RPM Rotor [Mtip] 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 0.623 2.0 2.0 Alfa -5.0 -3.7 -3.7 -5.5 -7.3 -7.3 -9.1 -5.5 -9.1 -9.1 -5.0 -5.0 -9.1 -9.1 -9.1 -9.3 (deg) -10.0 -10.0 -10.0 -10.0 -10.0 -10.0 -10.0 -15.0 -12.0 -10.0 -12.0 0.0, 2.4 0.0, 1.6 2.5, 5.0, 7.5 -15.0, -12.5, -5.0 0, 1, 2, 3, 4, 5, 6, 7 -3.9, -2, -1, 0, 1, 2.5 -5.5, -2.5, 0, 1.5, 2, 2.3, 2.5, 2.7, 3, 3.5, 4, 4.5, 5, Vkts [mu] 0.10 0.10 0.15 0.15 0.15 0.15 0.15 0.15 0.20 0.20 0.20 0.24 0.25 0.25 0.25 0.30 0.20 0.20 0.20 0.30 0.30 0.30 0.30 0.20 0.15 0.25 0.20 0.30 0.30 0.20 0.30 0.375 0.375 0.375 0.375 0.375 DESCRIPTION Summary of Specific Conditions Baseline cases with no flap inputs, i.e. 0V.

controls, +/-1 deg fwd; +/-1 deg rt baseline performance baseline performance controls, +/-1 deg fwd; +/-1 deg rt baseline performance baseline performance controls, +/-1 deg fwd; +/-1 deg rt baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance baseline performance alfa sweep for max BVI alfa sweep for max BVI alfa sweep for max BVI baseline performance performance w flap 0V and 0deg performance w flap 1.5deg 2P performance w flap 0V and 0deg performance w flap 1.5deg 2P performance w flap 0V and 0deg performance w flap 0V and 0deg 20 18 29 36 13-19 21-24 25-31 31-36 11-17 47-52 19-23 24,25 42-44 35,36 32-37 49-54 55-69 26-28 21-25 29-34 30-32 33-35 23-30 40-44 71-88 69-84 33-46 48-62 71-75 Points 36.01-37 29.01-31 26-27.03 85.01-98 34-37.02 69,70,76 29.03-29.05 Boeing Values 14 14 14 14 14 14 15 15 15 15 15 15 15 15 15 15 20 20 20 20 23 23 23 25 25 25 28 29 29 29 38 39 41 42 42 42 Run Appendix D—Baseline and Performance Test Conditions SMART Rotor Test Runs: Swashplate controls checkout baseline performance, alfa, CT sweeps alfa sweep for max BVI. Performance with flap inputs (runs 38–42); also listed in sheet “Flap.” RPCM problem, fast shut down? using 1-6P fpr position control for start up, overcome integrator limits by hand 200k limit hit 200k limit hit 390k limit hit start up controlled by software Heim recorder failed Heim recorder failed RPCM problem, ok after reboot SRH - data given to CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC also alfa=0.29, 1.49 Variables 0V; 150V, 0-200Hz; 200V, 0-80Hz; 0.2-5Hz, 2, 3, 4, 5, 6, 10P, sine 0V; 200,300,400V at 2P and 5P 0,200,300V at 3P60 0V; 200, 300, 400V 3P60 0V; 200,300,400V 5P90 0V; 350V 3P60 0V; 200V 2P240 +100V 5P330; 250V.. ; 300V.. 0V; 300, 350, 400V, 5P90 0V; 300,350,400V 3P60; 0V 0V; (200V, 0-80 lin, 1-80, 0.2-5Hz, 2,3,4,5,6,10P log), col, lon, lat 250V 4P; 0V 0V; (200V, 0.2-80Hz log), col, lon, lat, col 0V; (200V, 0-80 lin, 0.2-9 log, 5P lin), col, lon, lat; 0V 0V; 250V, 5P, 6P, 3P, 2P; 0V 0V; (200V, 0-80 lin, 0.2-9 log), col, lon, lat; 0V 0V; 250V 4P virt sp lat 0V; 0, 1, 1.5, 2d2P240+1d5P330; 0V; 0V; 250V 4P, 5P, 6P, 3P, 2P; 0V 0V, 0, 1, 2deg 3P60; 0V 0V; 0, 1, 2deg 5P90 0deg 1.5deg 2P90; (0V) 0V; (200V, 0-80Hz, lin), col, lon, lat 0V; 250-500V 2P90; 1.5d 2P90, +/-15 250-450V 3P240; 1.5d 3P240, +/-15 150-300V 4P90; 1.5d 4P90, +/-15 150-350V 5P0; 1.5d 5P0, +/-15 actuator check 2 0Vbias; 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 2 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 2 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 3 0V; 400, 100V 1Hz; 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 2 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 3 0V; 400, 100V 1Hz; 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 2 0V; 200V, 1,6P, harmonic, cyclic; 0V actuator check 3 0V, 0Vbias,zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 400V 5P; 0V actuator check 2 200V, 5,6P, harmonic, cyclic; 0V actuator check 3 0V; 400, 100V 1Hz; 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 2 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz actuator check 3 0V; 400, 100V 1Hz; 0Vbias; zero actuator check 1b 0deg; DARPA1-4; 0V actuator check 2b 0V; 0deg; DARPA1-4; 0V actuator check 2b 0V; 0d, 1d1P, 2d1P, 2d1P90; 0V actuator check 1,1b 0Vbias; 0V; 200,300,400V, 1Hz; 0d, 1d1P, 2d1P90; 0V Type actuator check rot stea0Vbias; 0V; V1,V2,V3,V4,V5=200; V=200, 300, 400, 0, -200, -300, -400, 0 freq sweep actuator check rot actuator check rot DARPA2, OL DARPA1, OL DARPA2, OL DARPA4, OL DARPA1, OL DARPA2, OL freq sweep phase sweep freq sweep freq sweep phase sweep freq sweep phase sweep DARPA4, CTC phase sweep DARPA2, CTC DARPA1, CTC phase sweep + ampl phase sweep + ampl phase sweep + ampl phase sweep + ampl trav sweep trav sweep freq sweep 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.3 0.3 0.3 0.3 0.2 0.3 0.3 0.3 0.3 0.3 0.3 0.2 0.2 0.2 0.2 0.3 0.3 0.2 0.2 0.2 0.2 0.2 0.2 0.3 Speed 2P90 3P240 4P90 5P0 col,log 0-6P 2P90,Trav13 Summary of Specific Conditions Cases with flap inputs, open and closed loop.

check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,400V1Hz check,Nr=0,COLL=10,ALF=0,400V1Hz check,Nr=0,COLL=10,ALF=0,400V1Hz check,Nr=0,COLL=10,ALF=0,400V1Hz Condition COLL=4,ALF=-10,VKTS=0 COLL=4,ALF=-10,MU=0,150V,0-200Hz,120sec COLL=4,ALF=-10,VKTS=0,df=200V1P CT/S=0.075,ALF=1.49,MU=0.2,df=200V2P Act COLL=4,ALF=-10,VKTS=0,df=200V1P CT/S=0.08,ALF=-9.4,VKTS=123,df=0V Act COLL=4,ALF=-10,VKTS=0,df=200V1P CT/S=0.08,ALF=-9.1,VKTS=123,df=200V5P90 CT/S=0.08,ALF=-9.1,VKTS=123,df=350V3P60 Act Act COLL=4,ALF=-10,VKTS=0,df=200V1P 0.075,1.49,83,df=200V 2P240 +100V 5P330 Act Act CT/S=0.08,ALF=-9.1,VKTS=123,df=300V5P90 CT/S=0.08,ALF=-9.1,VKTS=123,df=300V3P60 0.075,-9.1,0.3,df200V0-80,60s, col, lin Post-run check, COLL=10, Vbias=0 Act COLL=4,-10,0,df=200V.2-80,5*40s, COLL=4,ALF=-10,VKTS=0,df=200V5P 0.075,-9.1,0.3,df=200V0-80,5*40s,col,lin CT/S=0.075,ALF=-9.1,MU=0.3,df=250V5P Act Act COLL=4,ALF=-10,VKTS=0,df=200V1P 0.075,2,0.2,df=200V0-80,3*40s,col,lin 0.075,2,0.2,df=250V4P,virt sp lat Post-run check, COLL=10, Vbias=0 Act COLL=10,ALF=0,MU=0,df=0deg COLL=4,-10,0,df=0deg 0-6P, 0.075,0.89,83,df=2d2P240+1d5P330+0d0-6P CT/S=0.075,ALF=2,MU=0.2,df=250V4P CT/S=0.08,-9.4,123,df=2deg 3P60 +0d0-6P CT/S=0.08,-9.4,123,df=2deg 5P90 +0d0-6P Act Act COLL=4,-10,0,df=0deg 0-6P, CT/S=0.075,ALF=2,MU=0.2,df=250V CT/S=0.075,ALF=2,MU=0.2,df=250V CT/S=0.075,ALF=2,MU=0.2,df=250V CT/S=0.075,ALF=2,MU=0.2,df=250V CT/S=0.075,2,0.2,df=0deg 0-6P,Trav1 CT/S=0.075,2,0.2,df=1.5deg CT/S=0.075,ALF=-9.1,MU=0.3,df=0V,40s CT/S=0.08,ALF=-9.1,MU=0.3,df=0V COLL=4,ALF=-10,VKTS=0,df=200V1P CT/S=0.075,ALF=-9.1,MU=0.3,df=250V4P Points 8.02-23 86-101 7-15.01 44-46.02 69,70,70.01 3-8 11-18 36-39 3-8 11-18 22-25 33-43 64-68 3-8 11-18 22-25 136-140 3-8 11,12,17,18 38-41 49-60 61-85 86.01-98.01 143-147 3-9 12-16 17-19 23-30 30-84 108-112 3-9 12-19 44-51 51-64.01 123-127 3-7 8-13 16-22 26-34 35-102 104-109 109-114 119-123 3-11 14-19 23-32 51-59 60-68 78-86 96-108 109-122 124-130 Boeing Values Run 17 17 20 20 20 23 23 23 24 24 24 24 24 25 25 25 25 26 26 26 26 26 26 26 28 28 28 28 28 28 29 29 29 29 29 30 30 30 30 30 30 30 30 31 31 31 31 31 31 31 31 31 Appendix D—Active Flap Test Conditions (cont.) SMART Rotor Test Runs: using 1-5P for position control w/o Kalman filter up to pt 48 some df jumps at 1sec intervals from pt 50 Relax=0.5 helps to eliminate jumps point 7 w 400V has Vcmd=300V limit before this ASA pos always Upstream,U=-200 CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC HHC HHC HHC HHC HHC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC HHC HHC HHC HHC HHC CTC CTC CTC HHC 0V all at 0V all at 0V all at 0V all at 0V ASA pos at max BVI (-40) ASA pos at max BVI (-120) 0V; 200V, 0-80Hz, lin, col NF 5, 1, 1-5P; RM 5, 1, 1-5P; 0V 0V; 1.5deg 2P; 0V 0V; 1.5-3deg, 2P300, 90, 105; 0V 0Vbias; 0V; (175V col, 200V, lon, lat), 0-80Hz, lin 0V; NF 1-5P, PM 1-5P Mic1 5, 1-5P; 0V 0V; 1.5deg 3P; 0deg 0d; 1.5-2deg, 3P240, 230, 250; 0deg 0d; 1.5 deg 5P; 0deg 0d; 1-2deg, 5P80, 100, 70; 0V 0; (1, 2, 0, -1, -2) lon; 0; (1, 0, -1, -1) lat; Mic16 5, 1-5P; 0V 0V, 0, 1, 2deg 3P60; 0d 0d; 0, 1, 2deg 5P90; 0d; 0V 0V; (200V, 0.2-9Hz, log), col, lon, lat 0; (1,-1) col; 0; (1, 2, -1, -2) lon; 0;(1, -1) lat; 0; 0V; (250, -250V) col, lon, lat; 0deg 0d; (1,2,3,-1,-2,-3) col; 0d; (1,2,-1,-2,-3) lon; 0d; (1,2,3,-1,-2,-3) lat; 0d; 0V 0; (1,-1) col; 0; (1, 2, -1, -2) lon; 0;(1, -1) lat; 0; 0V; (250, -250V) col, lon, lat; 0deg 0d; (1,2,3,-1,-2,-3) col; 0d; (1,2,3,-1,-2,-3) lon; 0d; (1,2,3,-1,-2,-3) lat; 0d; HHC 0V; 0d; 1.5d 3, 4, 5, 2P ; 0d; 0d; 1-2.5deg, 3P180; 1,5deg (4P30, 5P300, 2P300) 1.5deg 3P180; 0deg (0V); 0deg 0d; 1.5deg 3, 4, 5, 2P; 0d; 0d; 1-2deg 4P30; 1.5deg 2P180, 3P150, 180, 4P60, 5P300 1.5deg 4P30; 0deg 0V; (150V col, 200V lon, 150V lat), 0.2-9Hz, log; 0V 0; (1,-1) col; 0; (1, 2, -1) lon; 0;(1, -1) lat; 0; 0V; (250, -250V) col, lon, lat; 0deg 0d; (1,2,3,-1,-2,-3) col; 0d; (1,2,-1,-2,-3) lon; 0d; (1,2,3,-1,-2,-3) lat; 0d; 0d; .7d3P258+.8d5P68; 0d 0d; 1d 4P; 1.5d 2P; 0d; .7d3P258+.8d5P68 ; 1.1d3P268+1d5P60; 0df; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 2b 0V; 0d, 1d1P, 2d1P; 0V actuator check 2b 0V; 0d, 1d1P, 2d1P actuator check 2b 0V; 0d, 1d1P, 2d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0V; 0d, 1d1P freq sweep vib control phase sweep phase sweep + ampl freq sweep vib control noise control phase sweep phase sweep + ampl phase sweep phase sweep + ampl control power SP noise control DARPA2, CTC DARPA1, CTC freq sweep control power SP control power VSP control power IBC control power SP control power VSP control power IBC phase sweep phase sweep + ampl trav sweep trav sweep phase sweep phase sweep + ampl trav sweep freq sweep control power SP control power VSP control power IBC noise control OL_opt phase sweep noise control OL_opt 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.2 0.2 0.2 0.2 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.15 0.15 0.15 0.15 +.8deg5P68 +.8deg5P68 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 COLL=4,ALF-10,MU0,df=0deg 0-6P CT/S=0.075,ALF=2,MU=0.2,df=200V0-80 CT/S=0.075+1deg,ALF=-5.5,MU=0.2,df=0V CT/S=0.075+1deg,ALF=2,MU=0.2,df=0V CT/S=0.075,ALF4,MU=0.15,df=1.5deg3P CT/S=0.075,ALF4,MU=0.15,df=1.5deg2P180 0.075,4,0.15,df=1.5deg4P30,Tr=-120 Post-run check, COLL=10, Vbias=0 COLL=4,ALF-10,MU0,df=0deg 0-6P 0.075,-9.1,0.3,150V0.2-9,3*40s,col,log CT/S=0.075+1deg,ALF=-9.1,MU=0.3,df=0V CT/S=0.075,ALF=-9.1,MU=0.3,df=250Vcol CT/S=0.075,ALF=-9.1,MU=0.3,df=1deg0P 0.075,-9.1,0.3,df=.7deg3P258 CT/S=0.075,ALF=-9.1,MU=0.3,df=1deg4P 0.075,-9.1,0.3,df=.7deg3P258 Post-run check, COLL=10, Vbias=0 Post-run check, COLL=10, Vbias=0 Act CT/S=0.075,ALF=2,MU=0.2,df=NF5P CT/S=0.075,ALF=2,MU=0.2,df=1.5deg2P CT/S=0.075,ALF=2,MU=0.2,df=1.5deg2P300 Post-run zero, COLL=10,Vbias=0 Act COLL=4,ALF-10,MU0,df=0deg 0-6P 0.075,-9.1,0.3,df=175V0-80,3*40s,col,lin CT/S=0.075,ALF=-9.1,MU=0.3,df=NF1-5P CT/S=0.075,ALF=-9.1,MU=0.3,df=Mic15P CT/S=0.075,ALF=-9.1,MU=0.3,df=1.5deg3P CT/S=0.075,ALF=-9.1,MU=0.3,df1.5deg3P240 CT/S=0.075,ALF=-9.1,MU=0.3,df=1.5deg5P CT/S=0.075,ALF=-9.1,MU=0.3,df=1.5deg5P90 CT/S=0.075,ALF=-9.1,MU=0.3,df=0V CT/S=0.075,ALF=-9.1,MU=0.3,df=Mic165P 0.08,-9.4,123,df=2deg 3P60 +0d0-6P 0.08,-9.4,123,df=2deg 5P90 +0d0-6P Post-run check, COLL=10 Act COLL=4,ALF-10,MU0,df=0deg 0-6P 0.075,-5.5,0.2,200V0.2-9,3*40s,col,log CT/S=0.075,ALF=-5.5,MU=0.2,df=250Vcol CT/S=0.075,ALF=-5.5,MU=0.2,df=1deg0P CT/S=0.075,ALF=2,MU=0.2,df=250Vcol CT/S=0.075,ALF=2,MU=0.2,df=1deg0P Post-run check, COLL=10, Vbias=0 Act COLL=4,ALF-10,MU0,df=0deg 0-6P CT/S=0.075,ALF=2,MU=0.2,df=1.5deg3P CT/S=0.075,ALF=2,MU=0.2,df=1.5deg3P180 0.075,2,0.2,df=1.5deg3P180,Tr=-200 Post-run check, COLL=10, Vbias=0 Act COLL=4,ALF-10,MU0,df=0deg 0-6P Act 135-139 3-9 12-17 21-22 23.01-32 32-46 46-81 126-127.01 3-8 11-14 17-22 22-26 27-30 30-44 44-52 52-66 66-74 74-84 102-105 106-112 112-116.01 124,125 3-8 11-14 17-21 21-32 32-39 39-60 72-83 83-90 90-111 118-120 3-8 11-15 17-72 72-81 82-82.29 94-96 3-8 11-13 16,98-111.06,10.075,4,0.15,df=0deg,Tr=-200 18.01-71 71-81.01 82-124 134-138 3-8 11-13 17-21 21-32 32-39 39-60 60.1-64 64-92 92-109.01 114-116 31 32 32 32 32 32 32 32 33 33 33 33 33 33 33 33 33 33 33 33 33 33 34 34 34 34 34 34 34 34 34 34 35 35 35 35 35 35 36 36 36 36 36 36 36 37 37 37 37 37 37 37 37 37 37

Appendix D—Active Flap Test Conditions (cont.)

Pt 24- controller instability Pt 58+ controller instability Pt 64 aborted SW error SW error SW error w AFC data SW error SW error SW error SW error CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC2 CTC CTC HHC HHC HHC HHC HHC HHC HHC HHC HHC HHC HHC HHC HHC HHC HHC HHC, CTC CTC CTC CTC3 coeff for 82kt CTC CTC CTC HHC HHC HHC HHC HHC HHC HHC ASA pos at max BVI Mic 9 (-80) ASA pos at max BVI (-120) ASA pos at max BVI Mic 9 (-80) 0d; 1d 3P250 + 1d 2P; 1d 3P250 + (1, .75, .5)d4P; 0d 0d; (1, 2, 3, -1, -2, -3) df1; (1, 2, 3, -1, -2, -3) df2 (CTS= .075, .040, .060, .080, .090, .075) 0deg, 0V, no retrim 0d; df1= 1, 2, 3, -1, -2, -3; 0V; 0d; df2= 1, 2, 3, -1, -2, -3; 0d 0V; 150V, 0-80Hz, lin, col 0V; NF1-5P, (T=10,1); PM 1-5P, (T=10,1); 0d 0d; 1.5d 2P phase sweep, w retrim; 0d; 0V (0V); 0d (0V); 0d 0d; 1.5d3P; 1.5d4P; 0d; 1.5d 3P180 (CTS= .075, .040, .060, .080, .090, .10, .075) 0deg, 0V, no retrim 0d; df1= 1, 2, 3, -1, -2, -3; 0d 0V; 150V, .2-200Hz, col, (log, lin); 200V, 0-80Hz, lin, col, lon, lat 0V; NF 10P, T=5,1; NF 1-5,10P, T=10,5 0d; 1.5d 2P phase sweep, w retrim; 0d 0d; [1.5d 5P180 - kill flaps] 75V,0-200Hz, lin, col 0V; 0d; 0.7-1.3d, 4P180, 170; 1-2d 2P0; 1d 3P250; 0d 0V; 0d; (1-2)d 3P250 +(1-2)d2P0; (.5-1.5)d 3P250 +(.5-1)d4P180; 0V 0d; 1,5d4P30; xd(2-5)Py; 0d; 0V; 1.5-2d, 3P165-180; 1.5d 4P120-180 0d; 1.5d 3P180; xdeg(2-5)Py; HHC vs CTC: 0d; 2d2P240+1d5P330 0d; 1.3d 4P180; [xdeg(2-5)Py - kill flaps] vib control 0d; NF 5P vib control 0d; NF, RM, PM 5P w 4, 5, 6P; 0V vib control 0V; NF; RM; 3F; NF,RM,PM; 0V; 0d vib control NF 5, 1-5P; RM 5, 1-5P noise control 0V; 250V 4P30; 0d; 1.5d 4P30; Mic1 noise control 0V; 250V 3P180; 0d; 1.5d 3P180; Mic1 noise control 0V; 225V 4P180; 0d; 1.3d 4P180; Mic13 actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 0Vbias; zero actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 3 0V, 200,300,400V; 75V 0-200Hz col, lin; 100V 1Hz; 0Vbias; zero actuator check 2b 0V; 0d, 1d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0V; 0d, 1d1P, 2d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0d; 1d1P actuator check 2b 0V; 0d, 1d1P phase sweep + ampl phase sweep rotor smoothing performance rotor smoothing phase sweep + ampl freq sweep vib control performance trav sweep noise control OL_opt trav sweep phase sweep phase sweep + ampl trav sweep noise control OL_opt performance rotor smoothing DARPA4, HHC,CTC freq sweep vib control noise control OL_opt performance DARPA3, CTC freq sweep 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.2 0.2 0.2 0.2 0.2 0.3 0.3 0.3 0.2 0.3 0.3 0.25 0.15 0.15 0.15 0.165 0.165 0.165 0.165 0.165 0.375 col,log +1deg2P0 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 Act COLL=4,ALF-10,MU0,df=0deg 0-6P CT/S=0.075,ALF=-9.1,MU=0.3,df=1deg4P180 0.075,-9.1,0.3,df=1deg 3P250 + 1deg2P0 CT/S=0.075,ALF=-9.1,MU=0.3,df1=1deg0P CT/S=0.075,ALF=-9.1,MU=0.3,df=0deg Post-run check, COLL=10, Vbias=0 Act COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF=-10,MU=0,df=1deg0P 0.075,-9.1,0.3,df=1deg3P250 0.075,-9.1,0.3,175V,150V0-80,3*40s,col,lin 0.075,1.8,0.165,df=1.5deg3P 0.075,1.8,0.165,df=NF,RM,PM5P,4,5,6P 0.075,1.8,0.165,df=1.5deg3P180 0.075,1.8,0.165,df=1.5deg3P180,Tr=-200 Post-run check, COLL=10, Vbias=0 Act COLL=4,ALF-10,MU0,df=0deg 0-6P CT/S=0.075,ALF=2,MU=0.2,df=NF5P5Pcol 0.075,2,0.2,df~.75deg 2-5P,OL_opt CT/S=0.075,ALF=2,MU=0.2,df=0deg CT/S=0.075,ALF=2,MU=0.2,df=1deg0P CT/S=0.07,ALF=-9.3,MU=155,df=0deg Post-run check, COLL=10, Vbias=0 Act COLL=4,ALF-10,MU0,df=0deg 0-6P 0.075,4,0.15,df=Mic1,4P,RMS 0.075,2,0.2,df=Mic1,4P,RMS 0.075,-9.1,0.3,df=Mic13,4P,RMS 0.075,-9.1,0.3,df=NF5P,5Pcol,Vc=300 10deg,0,0,75V0-200,3*40,col,lin Post-run check, COLL=10, Vbias=0 0.075,-9.1,0.3,dfNF1-5P,T=10 0.075,-9.1,0.3,df=1.5deg2P CT/S=0.075,ALF=-4,MU=0.25,df=0degTr=-200 Post-run check, COLL=10, Vbias=0 Act COLL=4,ALF-10,MU0,df=0deg 0-6P 0.075,4,0.15,df~.75deg 2-5P,OL_opt CT/S=0.075,ALF=4,MU=0.15,df=NF5P,5P 0.075,1.8,0.165,df=0deg,Tr=-200 0.075,0.89,83,df=2d2P240+1d5P330 Post-run check, COLL=10, Vbias=0 Act COLL=2,-10,0,150V.2-200,3*40s, COLL=4,ALF-10,MU0,df=0deg 0-6P 0.075,-9.1,0.3,df=NF10P,T=5 CT/S=0.075,ALF=-9.1,MU=0.3,df1.3deg4P180 CT/S=0.09,ALF=-9.1,MU=0.3,df=1.5deg2P 3-8 11-13 17-29 29-57 57-71 71-88 103-105 3-8 11-13 14-28 49-63 63,64,6401 63,65-69 69-84 97-110 117-119 3-8 11-14 18-24 24-25 32-52 52-79 79-81 81-89 93-108 152-154 3-8 11-13 15.01-27 27-32 33-46 47-54 55.01-61 114-116 3-8 11-15 16,17 20-36 39,40, [41-47] 48-62 71-76 92-94 3-8 11-13 16-23.02 36-43.01 61-68.01 69-72 108 111-113 38 38 38 38 38 38 38 39 39 39 39 39 39 39 39 39 40 40 40 40 40 40 40 40 40 40 41 41 41 41 41 41 41 41 42 42 42 42 42 42 42 42 43 43 43 43 43 43 43 43

Appendix D—Active Flap Test Conditions (cont.)

RPCM problem, fast shut down? using 1-6P fpr position control using 1-5P for position control point 7 w 400V has Vcmd=300V limit for start up, overcome integrator limits by hand start up controlled by software w/o Kalman filter CTC CTC CTC HHC CTC CTC CTC CTC CTC CTC CTC HHC CTC CTC HHC CTC CTC HHC HHC CTC HHC CTC CTC CTC HHC HHC HHC CTC HHC Variables actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 400V 5P; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 1 0Vbias; 0V; 200,300,400V, 1Hz; 0V actuator check 2 0Vbias; 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 2 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 2 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 2 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 2 0V; 200V, 1,6P, harmonic, cyclic; 0V actuator check 2 200V, 5,6P, harmonic, cyclic; 0V actuator check 2 0V; 200V, 1-6P, harmonic, cyclic; 0V actuator check 3 0V; 400, 100V 1Hz; 0Vbias; zero actuator check 3 0V; 400, 100V 1Hz; 0Vbias; zero actuator check 3 0V, 0Vbias,zero actuator check 3 0V; 400, 100V 1Hz; 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V; 400, 100V 1Hz; 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 0Vbias actuator check 3 0V, 0Vbias; zero actuator check 1b 0deg; DARPA1-4; 0V actuator check 2b 0V; 0deg; DARPA1-4; 0V actuator check 2b 0V; 0d, 1d1P, 2d1P, 2d1P90; 0V actuator check 2b 0V; 0d, 1d1P, 2d1P; 0V actuator check 2b 0V; 0d, 1d1P, 2d1P actuator check 2b 0V; 0d, 1d1P, 2d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0V; 0d, 1d1P, 2d1P actuator check 2b 0V; 0d, 1d1P actuator check 2b 0d; 1d1P actuator check 2b 0V; 0d, 1d1P actuator check 1,1b 0Vbias; 0V; 200,300,400V, 1Hz; 0d, 1d1P, 2d1P90; 0V Type 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Speed 0-6P check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,Vbias=400 check,Nr=0,COLL=10,ALF=0,400V1Hz check,Nr=0,COLL=10,ALF=0,400V1Hz check,Nr=0,COLL=10,ALF=0,400V1Hz check,Nr=0,COLL=10,ALF=0,400V1Hz Condition Act Act Act Act Act Act Act Act Act Act Act Act Act Act Act Act Act Act Act Act COLL=10,ALF=0,MU=0,df=0deg COLL=4,ALF=-10,VKTS=0,df=200V1P COLL=4,ALF=-10,VKTS=0,df=200V1P COLL=4,ALF=-10,VKTS=0,df=200V1P COLL=4,ALF=-10,VKTS=0,df=200V1P COLL=4,ALF=-10,VKTS=0,df=200V1P COLL=4,ALF=-10,VKTS=0,df=200V5P COLL=4,ALF=-10,VKTS=0,df=200V1P COLL=4,-10,0,df=0deg 0-6P, COLL=4,-10,0,df=0deg 0-6P, COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P COLL=4,ALF-10,MU0,df=0deg 0-6P Act Act Post-run check, COLL=10, Vbias=0 Act Post-run check, COLL=10, Vbias=0 Act Post-run check, COLL=10, Vbias=0 Post-run zero, COLL=10,Vbias=0 Post-run check, COLL=10 Post-run check, COLL=10, Vbias=0 -8 3-7 3-9 3-8 3-8 3-8 3-8 3-8 3-8 3-8 3-8 3-8 3-8 3-8 3-11 7-15.01 11-18 11-18 11-18 11,12,17,18 17-19 12-17 11-14 11-14 11-15 11-13 11-13 11-13 11-13 11-14 11-13 16,17 11-13 64-68 136-140 143-147 108-112 123-127 119-123 135-139 Points 3 3-8 3-8 3-8 3-9 3-9 8-13 12-19 16-22 14-19 126-127.01 124,125 118-120 Boeing Values Run 23 24 25 26 28 29 30 32 33 34 35 36 37 38 39 40 41 42 43 31 30 20 23 24 25 26 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 24 25 26 28 29 30 31 32 33 34 Appendix D—Active Flap Test Conditions (cont.) SMART Rotor Test Runs: Summary of Specific Conditions Cases with flap inputs, open and closed loop.

from pt 50 Relax=0.5 helps to eliminate jumps 390k limit hit 200k limit hit 200k limit hit RPCM problem, ok after reboot up to pt 48 some df jumps at 1sec intervals Pt 64 aborted w AFC data SW error SW error SW error HHC HHC HHC CTC CTC CTC CTC CTC CTC HHC, CTC SRH - data given to CTC CTC HHC HHC CTC HHC CTC CTC HHC HHC HHC CTC CTC HHC HHC all at 0V all at 0V all at 0V all at 0V also alfa=0.29, 1.49 0V; 200,300,400V at 2P and 5P 0,200,300V at 3P60 0d; (1,2,3,-1,-2,-3) col; 0d; (1,2,-1,-2,-3) lon; 0d; (1,2,3,-1,-2,-3) lat; 0d; 0V 0d; (1,2,3,-1,-2,-3) col; 0d; (1,2,3,-1,-2,-3) lon; 0d; (1,2,3,-1,-2,-3) lat; 0d; HHC 0d; (1,2,3,-1,-2,-3) col; 0d; (1,2,-1,-2,-3) lon; 0d; (1,2,3,-1,-2,-3) lat; 0d; 0V 0; (1, 2, 0, -1, -2) lon; 0; (1, 0, -1, -1) lat; 0; (1,-1) col; 0; (1, 2, -1, -2) lon; 0;(1, -1) lat; 0; 0; (1,-1) col; 0; (1, 2, -1, -2) lon; 0;(1, -1) lat; 0; 0; (1,-1) col; 0; (1, 2, -1) lon; 0;(1, -1) lat; 0; 0V; (250, -250V) col, lon, lat; 0deg 0V; (250, -250V) col, lon, lat; 0deg 0V; (250, -250V) col, lon, lat; 0deg 0V; 0, 1, 2deg 5P90 0d; 0, 1, 2deg 5P90; 0d; 0V 0V; 200,300,400V 5P90 0V; 300, 350, 400V, 5P90 0V, 0, 1, 2deg 3P60; 0V 0V, 0, 1, 2deg 3P60; 0d 0V; 200, 300, 400V 3P60 0V; 350V 3P60 0V; 300,350,400V 3P60; 0V 0d; [1.5d 5P180 - kill flaps] 0V; 0, 1, 1.5, 2d2P240+1d5P330; 0V; 0V; 200V 2P240 +100V 5P330; 250V.. ; 300V.. 0V; 150V, 0-200Hz; 200V, 0-80Hz; 0.2-5Hz, 2, 3, 4, 5, 6, 10P, sine 0V; (200V, 0-80 lin, 1-80, 0.2-5Hz, 2,3,4,5,6,10P log), col, lon, lat 0V; (200V, 0.2-80Hz log), col, lon, lat, col 0V; (200V, 0-80 lin, 0.2-9 log, 5P lin), col, lon, lat; 0V 0V; (200V, 0-80 lin, 0.2-9 log), col, lon, lat; 0V 0V; (200V, 0-80Hz, lin), col, lon, lat 0V; 200V, 0-80Hz, lin, col 0Vbias; 0V; (175V col, 200V, lon, lat), 0-80Hz, lin 0V; (200V, 0.2-9Hz, log), col, lon, lat 0V; (150V col, 200V lon, 150V lat), 0.2-9Hz, log; 0V 0V; 150V, 0-80Hz, lin, col 0V; 150V, .2-200Hz, col, (log, lin); 200V, 0-80Hz, lin, col, lon, lat 75V,0-200Hz, lin, col Mic1 5, 1-5P; 0V Mic16 5, 1-5P; 0V HHC vs CTC: 0d; 2d2P240+1d5P330 0d; .7d3P258+.8d5P68; 0d 0d; .7d3P258+.8d5P68 ; 1.1d3P268+1d5P60; 0df; 0V noise control 0V; 250V 4P30; 0d; 1.5d 4P30; Mic1 noise control 0V; 250V 3P180; 0d; 1.5d 3P180; Mic1 noise control 0V; 225V 4P180; 0d; 1.3d 4P180; Mic13 actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 0Vbias; zero actuator check 3 0V, 200,300,400V; 75V 0-200Hz col, lin; 100V 1Hz; 0Vbias; zero actuator check rot actuator check rot actuator check rot stea0Vbias; 0V; V1,V2,V3,V4,V5=200; V=200, 300, 400, 0, -200, -300, -400, 0 control power IBC control power IBC control power IBC control power SP control power SP control power SP control power SP control power VSP control power VSP control power VSP DARPA1, CTC DARPA1, CTC DARPA1, OL DARPA1, OL DARPA2, CTC DARPA2, CTC DARPA2, OL DARPA2, OL DARPA2, OL DARPA3, CTC DARPA4, CTC DARPA4, HHC,CTC DARPA4, OL freq sweep freq sweep freq sweep freq sweep freq sweep freq sweep freq sweep freq sweep freq sweep freq sweep freq sweep freq sweep freq sweep noise control noise control noise control OL_opt noise control OL_opt 0 0 0 0 0 0 0 0 0 0 0 0 0.3 0.2 0.2 0.3 0.3 0.2 0.2 0.3 0.2 0.2 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.2 0.2 0.2 0.3 0 0.3 0.2 0.3 0.2 0.3 0.2 0.3 0.3 0 0 0.3 0.3 0.2 0.3 0.3 0.3 0.15 0.375 +.8deg5P68 +.8deg5P68 Post-run check, COLL=10, Vbias=0 Post-run check, COLL=10, Vbias=0 Post-run check, COLL=10, Vbias=0 Post-run check, COLL=10, Vbias=0 Post-run check, COLL=10, Vbias=0 Post-run check, COLL=10, Vbias=0 Post-run check, COLL=10, Vbias=0 Post-run check, COLL=10, Vbias=0 Post-run check, COLL=10, Vbias=0 CT/S=0.075,ALF=1.49,MU=0.2,df=200V2P COLL=4,ALF=-10,VKTS=0 CT/S=0.075,ALF=-5.5,MU=0.2,df=1deg0P CT/S=0.075,ALF=2,MU=0.2,df=1deg0P CT/S=0.075,ALF=-9.1,MU=0.3,df=1deg0P CT/S=0.075,ALF=-9.1,MU=0.3,df=0V CT/S=0.075+1deg,ALF=-5.5,MU=0.2,df=0V CT/S=0.075+1deg,ALF=2,MU=0.2,df=0V CT/S=0.075+1deg,ALF=-9.1,MU=0.3,df=0V CT/S=0.075,ALF=-5.5,MU=0.2,df=250Vcol CT/S=0.075,ALF=2,MU=0.2,df=250Vcol CT/S=0.075,ALF=-9.1,MU=0.3,df=250Vcol CT/S=0.08,-9.4,123,df=2deg 5P90 +0d0-6P CT/S=0.08,ALF=-9.1,VKTS=123,df=200V5P90 CT/S=0.08,ALF=-9.1,VKTS=123,df=300V5P90 CT/S=0.08,-9.4,123,df=2deg 3P60 +0d0-6P 0.08,-9.4,123,df=2deg 3P60 +0d0-6P CT/S=0.08,ALF=-9.4,VKTS=123,df=0V CT/S=0.08,ALF=-9.1,VKTS=123,df=350V3P60 CT/S=0.08,ALF=-9.1,VKTS=123,df=300V3P60 CT/S=0.07,ALF=-9.3,MU=155,df=0deg 0.075,0.89,83,df=2d2P240+1d5P330+0d0-6P 0.075,0.89,83,df=2d2P240+1d5P330 0.075,1.49,83,df=200V 2P240 +100V 5P330 COLL=4,ALF=-10,MU=0,150V,0-200Hz,120sec 0.075,-9.1,0.3,df200V0-80,60s, col, lin COLL=4,-10,0,df=200V.2-80,5*40s, col,log 0.075,-9.1,0.3,df=200V0-80,5*40s,col,lin 0.075,2,0.2,df=200V0-80,3*40s,col,lin CT/S=0.075,ALF=-9.1,MU=0.3,df=0V,40s CT/S=0.075,ALF=2,MU=0.2,df=200V0-80 0.075,-9.1,0.3,df=175V0-80,3*40s,col,lin 0.075,-5.5,0.2,200V0.2-9,3*40s,col,log 0.075,-9.1,0.3,150V0.2-9,3*40s,col,log 0.075,-9.1,0.3,175V,150V0-80,3*40s,col,lin COLL=2,-10,0,150V.2-200,3*40s, col,log 10deg,0,0,75V0-200,3*40,col,lin CT/S=0.075,ALF=-9.1,MU=0.3,df=Mic15P CT/S=0.075,ALF=-9.1,MU=0.3,df=Mic165P 0.075,4,0.15,df=Mic1,4P,RMS 0.075,2,0.2,df=Mic1,4P,RMS 0.075,-9.1,0.3,df=Mic13,4P,RMS 0.075,-9.1,0.3,df=.7deg3P258 0.075,-9.1,0.3,df=.7deg3P258 CT/S=0.08,ALF=-9.1,MU=0.3,df=0V 0.08,-9.4,123,df=2deg 5P90 +0d0-6P 94-96 134-138 114-116 103-105 117-119 152-154 114-116 92-94 111-113 44-46.02 69,70,70.01 8.02-23 39-60 90-111 39-60 74-84 21-32 72-83 21-32 32-39 83-90 32-39 109-114 112-116.01 22-25 38-41 104-109 106-112 36-39 33-43 49-60 71-76 26-34 55.01-61 22-25 86-101 61-85 12-16 23-30 44-51 124-130 21-22 17-22 17-21 17-21 63,64,6401 11-15 108 27-30 102-105 16-23.02 36-43.01 61-68.01 60.1-64 92-109.01 35 36 37 38 39 40 41 42 43 20 17 34 34 37 33 34 37 34 34 37 30 33 24 26 30 33 23 24 26 42 30 41 25 17 26 28 31 33 34 39 33 33 43 43 43 37 37

Appendix D—Active Flap Test Conditions (cont.)

39 40 42 38 Pt 58+ controller instability Heim recorder failed SW error SW error SW error SW error before this ASA pos always Upstream,U=-200 Heim recorder failed 41 26 Pt 24- controller instability CTC HHC HHC CTC CTC CTC HHC CTC CTC CTC CTC CTC CTC CTC CTC HHC CTC CTC CTC CTC CTC CTC CTC CTC CTC CTC HHC CTC CTC HHC CTC CTC CTC CTC CTC CTC HHC HHC CTC CTC CTC2 HHC HHC HHC CTC3 coeff for 82kt HHC ASA pos at max BVI Mic 9 (-80) ASA pos at max BVI (-120) ASA pos at max BVI (-40) ASA pos at max BVI (-120) ASA pos at max BVI Mic 9 (-80) 0V; 0d; (1-2)d 3P250 +(1-2)d2P0; (.5-1.5)d 3P250 +(.5-1)d4P180; 0V 0d; NF, RM, PM 5P w 4, 5, 6P; 0V (CTS= .075, .040, .060, .080, .090, .075) 0deg, 0V, no retrim 0d; 1.5d 2P phase sweep, w retrim; 0d; 0V (CTS= .075, .040, .060, .080, .090, .10, .075) 0deg, 0V, no retrim 0d; 1.5d 2P phase sweep, w retrim; 0d 250V 4P; 0V 0V; 250V, 5P, 6P, 3P, 2P; 0V 0V; 250V 4P virt sp lat 0V; 250V 4P, 5P, 6P, 3P, 2P; 0V 0V; 1.5deg 2P; 0V 0V; 1.5deg 3P; 0deg 0d; 1.5 deg 5P; 0deg 0V; 0d; 1.5d 3, 4, 5, 2P ; 0d; 0d; 1.5deg 3, 4, 5, 2P; 0d; 0d; 1d 4P; 1.5d 2P; 0d; 1d 3P250 + 1d 2P; 1d 3P250 + (1, .75, .5)d4P; 0d 0d; 1.5d3P; 1.5d4P; 0d; 0d; (1, 2, 3, -1, -2, -3) df1; (1, 2, 3, -1, -2, -3) df2 0d; df1= 1, 2, 3, -1, -2, -3; 0V; 0d; df2= 1, 2, 3, -1, -2, -3; 0d 0d; df1= 1, 2, 3, -1, -2, -3; 0d 0deg 1.5deg 2P90; (0V) 1.5deg 3P180; 0deg (0V); 0deg 1.5deg 4P30; 0deg (0V); 0d (0V); 0d 1.5d 3P180 NF 5, 1, 1-5P; RM 5, 1, 1-5P; 0V 0V; NF 1-5P, PM 1-5P 0V; NF1-5P, (T=10,1); PM 1-5P, (T=10,1); 0d 0V; NF 10P, T=5,1; NF 1-5,10P, T=10,5 0V; 250-500V 2P90; 1.5d 2P90, +/-15 250-450V 3P240; 1.5d 3P240, +/-15 150-300V 4P90; 1.5d 4P90, +/-15 150-350V 5P0; 1.5d 5P0, +/-15 0V; 1.5-3deg, 2P300, 90, 105; 0V 0d; 1.5-2deg, 3P240, 230, 250; 0deg 0d; 1-2deg, 5P80, 100, 70; 0V 0d; 1-2.5deg, 3P180; 1,5deg (4P30, 5P300, 2P300) 0d; NF 5P 0d; 1,5d4P30; xd(2-5)Py; 0d; 0d; 1.5d 3P180; xdeg(2-5)Py; 0d; 1.3d 4P180; [xdeg(2-5)Py - kill flaps] 0d; 1-2deg 4P30; 1.5deg 2P180, 3P150, 180, 4P60, 5P300 0V; 1.5-2d, 3P165-180; 1.5d 4P120-180 0V; 0d; 0.7-1.3d, 4P180, 170; 1-2d 2P0; 1d 3P250; 0d NF 5, 1-5P; RM 5, 1-5P 0V; NF; RM; 3F; NF,RM,PM; 0V; 0d vib control vib control performance performance performance phase sweep phase sweep phase sweep phase sweep + ampl phase sweep + ampl rotor smoothing noise control OL_opt noise control OL_opt noise control OL_opt performance phase sweep phase sweep phase sweep phase sweep phase sweep phase sweep phase sweep phase sweep phase sweep phase sweep + ampl phase sweep + ampl phase sweep + ampl phase sweep + ampl phase sweep + ampl phase sweep + ampl phase sweep + ampl phase sweep + ampl phase sweep + ampl rotor smoothing rotor smoothing trav sweep trav sweep trav sweep trav sweep trav sweep trav sweep trav sweep vib control vib control vib control vib control vib control vib control phase sweep + ampl trav sweep 0.2 0.3 0.3 0.3 0.2 0.3 0.3 0.3 0.2 0.2 0.2 0.3 0.3 0.3 0.3 0.2 0.2 0.2 0.2 0.2 0.3 0.3 0.2 0.3 0.2 0.2 0.2 0.2 0.2 0.3 0.3 0.2 0.3 0.3 0.15 0.2 0.15 0.15 0.15 0.15 0.165 0.3 0.3 0.165 0.165 0.165 0.15 0.165 0.25 2P90 3P240 4P90 5P0 2P90,Trav13 CT/S=0.075,ALF=2,MU=0.2,df=250V CT/S=0.075,ALF=-9.1,MU=0.3,df=1deg4P180 0.075,4,0.15,df~.75deg 2-5P,OL_opt 0.075,2,0.2,df~.75deg 2-5P,OL_opt CT/S=0.075,ALF=-9.1,MU=0.3,df=0deg 0.075,-9.1,0.3,df=1.5deg2P CT/S=0.075,ALF=2,MU=0.2,df=0deg CT/S=0.09,ALF=-9.1,MU=0.3,df=1.5deg2P CT/S=0.075,ALF=-9.1,MU=0.3,df=250V5P CT/S=0.075,ALF=2,MU=0.2,df=250V4P CT/S=0.075,ALF=2,MU=0.2,df=1.5deg2P CT/S=0.075,ALF=-9.1,MU=0.3,df=1.5deg3P CT/S=0.075,ALF=-9.1,MU=0.3,df=1.5deg5P CT/S=0.075,ALF=2,MU=0.2,df=1.5deg3P CT/S=0.075,ALF4,MU=0.15,df=1.5deg3P CT/S=0.075,ALF=-9.1,MU=0.3,df=1deg4P 0.075,-9.1,0.3,df=1deg 3P250 + 1deg2P0 0.075,1.8,0.165,df=1.5deg3P CT/S=0.075,ALF=2,MU=0.2,df=250V CT/S=0.075,ALF=2,MU=0.2,df=250V CT/S=0.075,ALF=2,MU=0.2,df=250V CT/S=0.075,ALF=2,MU=0.2,df=1.5deg2P300 CT/S=0.075,ALF=-9.1,MU=0.3,df1.5deg3P240 CT/S=0.075,ALF=-9.1,MU=0.3,df=1.5deg5P90 CT/S=0.075,ALF=2,MU=0.2,df=1.5deg3P180 0.075,-9.1,0.3,df=1deg3P250 +1deg2P0 0.075,1.8,0.165,df=1.5deg3P180 CT/S=0.075,ALF=-9.1,MU=0.3,df1=1deg0P COLL=4,ALF=-10,MU=0,df=1deg0P CT/S=0.075,ALF=2,MU=0.2,df=1deg0P CT/S=0.075,2,0.2,df=0deg 0-6P,Trav1 CT/S=0.075,2,0.2,df=1.5deg 0.075,4,0.15,df=1.5deg4P30,Tr=-120 CT/S=0.075,ALF=-4,MU=0.25,df=0degTr=-200 0.075,1.8,0.165,df=0deg,Tr=-200 0.075,1.8,0.165,df=1.5deg3P180,Tr=-200 CT/S=0.075,ALF=-9.1,MU=0.3,df=NF1-5P CT/S=0.075,ALF=4,MU=0.15,df=NF5P,5P 0.075,1.8,0.165,df=NF,RM,PM5P,4,5,6P 0.075,-9.1,0.3,df=NF10P,T=5 0.075,-9.1,0.3,df=NF5P,5Pcol,Vc=300 CT/S=0.075,ALF=-9.1,MU=0.3,df=250V4P 0.075,2,0.2,df=250V4P,virt sp lat CT/S=0.075,ALF4,MU=0.15,df=1.5deg2P180 0.075,2,0.2,df=1.5deg3P180,Tr=-200 CT/S=0.075,ALF=2,MU=0.2,df=NF5P 0.075,-9.1,0.3,dfNF1-5P,T=10 CT/S=0.075,ALF=2,MU=0.2,df=NF5P5Pcol 18-24 27-32 69-84 33-46 48-62 86.01-98.01 30-84 35-102 32-46 30-44 52-66 17-72 18.01-71 64-92 29-57 52-79 23-32 51-59 60-68 78-86 46-81 44-52 66-74 72-81 17-29 57-71 14-28 47-54 96-108 109-122 82-124 97-110 32-52 93-108 22-26 24-25 79-81 15.01-27 20-36 69-72 51-64.01 71-81.01 82-82.29 16,98-111.06,10.075,4,0.15,df=0deg,Tr=-200 23.01-32 63,65-69 40 41 39,40, [41-47] CT/S=0.075,ALF=-9.1,MU=0.3,df1.3deg4P180 71-88 39 42 28 29 30 32 33 33 35 37 38 40 31 31 31 32 33 33 35 36 38 49-63 81-89 38 39 41 31 31 35 36 36 39 40 40 32 33 39 40 41 42 43

Appendix D—Active Flap Test Conditions (concluded)

Appendix E—Photographs Feb 13–May 2, 2008 SMART ROTOR TEST IN THE 40- X 80-FOOT WIND TUNNEL Unigraphics CAD Model Computational Aero-Acoustics SMART ROTOR—GEOMETRY Whirl Tower Test HQP - Smart Rotor Test Data PC 1 Control Room Amplifiers, HMS, Rotor Control Data PC 2 Rotating Data System P - Smart Rotor Test HQ PCM Data Display Data PC 1—Displays 3 and 4 Display Display 6 Display 5 Data PC 2—Displays 5 and 6 Control Room AFC, Flap Control & Data Acqu., Data PC2, Data PC1 RCC, Motor Control, Test Conditions, Tunnel Control BDM Targets SMART ROTOR IN THE 40- X 80-FOOT WIND TUNNEL

SMART ROTOR IN THE 40- X 80-FOOT WIND TUNNEL

SMART ROTOR IN THE 40- X 80-FOOT WIND TUNNEL