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Determining Aircraft Moments of Inertia from Flight Test Data

· NASA (NTRS) · 2020

Public domain · NASA (NTRS)Technical Reports

Overview

Flight test maneuver design and dynamic modeling techniques were developed for determining aircraft moments of inertia from flight test data. Full nonlinear rigid-body rotational equations of motion were used in the analysis, with aerodynamic moment dependencies modeled by linear expansions in the…

Publisher
NASA (NTRS)
Document
Year
2020
Pages
18

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Inputs

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domains trajectory and coverage flight good varied nominal frequency tests and off amplitudes and domain

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Document details

Doc number
Publisher
NASA (NTRS)
Year
2020
Pages
18
File size
492 KB