Two Reconfigurable Flight-Control Design Methods: Robust Servomechanism and Control Allocation
- 1 May 2001
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 24 (3) , 482-493
- https://doi.org/10.2514/2.4769
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Model following reconfigurable flight control system for the AFTI/F-16Journal of Guidance, Control, and Dynamics, 1990