Functional control law design using exact non-linear dynamic inversion-Reference-Cited by-同舟云学术

Functional control law design using exact non-linear dynamic inversion

Published:1994-08-01 Issue: Volume: Page:
ISSN:
Container-title:19th Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Smith P.¹

Affiliation:

1. Defence Research Agency, Bedford, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3516

Reference8 articles.

1. MortonBG,ElgersmaMR, HarveyCA,HarveyC A, Hines G, ' Nonlinear Flying Quality Parameters BasedonDynamicInversion',AFWAL-TR-87-3079, FlightDynamicsLab,Wright-PattersonAFB

2. SnellSA,EnnsDF and GarrardW LJr, 'Nonlinear InversionFlight ControlFor A Supermaneuverable Aircraft', AIAA Guidance Navigation and Control Conference,August 1990,pp808-825

3. Navigationandcontrolconference,August 1990,pp

4. 210-222

5. Conference,August 1993,pp 701-709

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