Dynamic inversion-based adaptive/reconfigurable control of the X-33 on ascent

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 2, 2002, Pages 275-284

  Doman, David B ^a   Ngo, Anhtuan D ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM ANALYSIS; ERROR ANALYSIS; HYPERSONIC AERODYNAMICS; IDENTIFICATION (CONTROL SYSTEMS); NONLINEAR CONTROL SYSTEMS; ONLINE SYSTEMS;

DYNAMIC INVERSION;

ADAPTIVE CONTROL SYSTEMS;

EID: 0036494418     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4879     Document Type: Article

References (10)

1. A self-designing receding horizon optimal flight controller
2. Nonlinear simulation analysis of a tailless advanced fighter aircraft with reconfigurable flight control law
3. Indirect adaptive flight control of a tailless fighter aircraft
4. System identification for adaptive and reconfigurable control
5. Adaptive flight control using dynamic inversion and neural networks
6. X-33 attitude control system design for ascent, transition, and entry flight regimes
7. Integration of online system identification and optimization-based control allocation
8. Fast control allocation using spherical coordinates