A type two trajectory linearization controller for a reusable launch vehicle - A singular perturbation approach

Collection of Technical Papers - AIAA Atmospheric Flight Mechanics Conference

Volumn 2, Issue , 2004, Pages 1121-1137

  Zhu, J Jim ^a   Huizenga, Andrew B ^a  

^a Ohio University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL DESIGNS; DESIGN TECHNIQUES; FLIGHT TRAJECTORY; LAUNCH VEHICLES;

AIRFRAMES; FLIGHT DYNAMICS; INTERPOLATION; LAUNCHING; LINEARIZATION; MANEUVERABILITY; PERTURBATION TECHNIQUES; ROBUSTNESS (CONTROL SYSTEMS); TRAJECTORIES;

AEROSPACE VEHICLES;

EID: 19644389286     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. John M. Hanson, "Advanced Guidance and Control Project for Reusable Launch Vehicles," 2000 AIAA Guidance, Navigation, and Control Conference, Denver, CO, Aug. 2000.
2. Yuri Shtessel and Charles Hall, "Reusable Launch Vehicle Control in Multiple Time Scale Sliding Modes," 2000 AIAA Guidance, Navigation, and Control Conference, Denver, CO, Aug. 2000.
3. A. J. Cause, E. Johnson, and H. El-Shirbiny, "An Adaptive Flight Control System Design for the X-33 Vehicle," 2000 AIAA Guidance, Navigation, and Control Conference, Denver, CO, Aug. 2000.
4. David B. Doman, David Leggett, and Mark Mears, "Development of a Hybrid Direct-Indirect Adaptive Control System for the X-33," 2000 AIAA Guidance, Navigation, and Control Conference, Denver, CO, Aug. 2000.
5. A. Scottedward Hodel, "Convex Programming in the Design of a Control System for a Reusable Launch Vehicle," 2000 AIAA Guidance, Navigation, and Control Conference, Denver, CO, Aug. 2000.
6. R. Smith, A. Ahmed, F.Y. Hadaegh, "The Design of a Robust Parametrically Varying Attitude Controller for the X-33 Vehicle," 2000 AIAA Guidance, Navigation, and Control Conference, Denver, CO, Aug. 2000.
7. C. E. Hall, M. W. Gallaher, N. D. Hendrix, "X-33 Attitude Control System Design for Ascent, Transition and Entry Flight Regimes," Proceedings of AIAA GNC Conference, Boston, MA, August, 1998.
8. C. E. Hall and H. Panossion, "X-33 Attitude Control Using the XRS-2000 Linear Aerospike Engine," Proceedings of the 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, June, 1999.
9. J. Zhu, Nonlinear Tracking and Decoupling by Trajectory Linearization, Lecture Note, Presented at NASA Marshall Space Flight Center, 137 pp., June 1998.