Nonlinear simulation analysis of a tailless advanced fighter aircraft reconfigurable flight control law
- 9 August 1999
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Parameter identification for systems with redundant actuatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Direct adaptive reconfigurable control of a tailless fighter aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Flight control reconfiguration on sliding modesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Multilayer neural networks and adaptive nonlinear control of agile anti-air missilesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Implementation and flight test assessment of an adaptive, reconfigurable flight control systemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Multiple control effector rate limitingJournal of Guidance, Control, and Dynamics, 1996
- System identification for adaptive and reconfigurable controlJournal of Guidance, Control, and Dynamics, 1995
- A dynamic inversion based control law with application to the high angle-of-attack research vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990