Adaptive guidance and control for autonomous launch vehicles

IEEE Aerospace Conference Proceedings

Volumn 6, Issue , 2001, Pages 2669-2682

  Johnson, E N ^a   Calise, A J ^a   Corban, J E ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPUTER SIMULATION; ELECTRONIC GUIDANCE SYSTEMS; MISSILE LAUNCHING SYSTEMS; PERTURBATION TECHNIQUES;

ADAPTIVE GUIDANCE; AUTOMONOUS LAUNCH VEHICLES;

ADAPTIVE CONTROL SYSTEMS;

EID: 0034855612     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Advanced guidance and control project for reusable launch vehicles
2. Development of a reconfigurable flight control law for the X-36 tailless fighter aircraft
3. Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft
4. Feedback linearization with neural network augmentation applied to X-33 attitude control
5. Design and evaluation of a 3-D optimal ascent guidance algorithm
6. Optimization of launch vehicle ascent trajectories with path constraints and coast arcs
7. Ascent, transition, entry, and abort guidance algorithm design for X-33 vehicle