Robust nonlinear dynamic inversion method for an aircraft motion control
Author:
Affiliation:
1. TsAGI, Zhukovsky, Russia; De Montfort Univ., Bedford, United Kingdom
2. TsAGI, Zhukovsky, Russia
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4208
Reference16 articles.
1. Flight control design using non-linear inverse dynamics
2. Nonlinear control law with application to high angle-of-attack flight
3. Invertibility and trajectory control for nonlinear maneuvers of aircraft
4. Balas G.J., Garrard W.L. and J.Reiner "Robust Dynamic Inversion Control Laws for Aircraft Control", AIAA-92-4329-CP.
5. Snell S.A. "Preliminary Assessment of the Robustness ofDynamicInversion Based Flight Control Laws", AIAA-92-4330-CP.
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