Multiple time scale sliding mode control of reusable launch vehicles in ascent and descent modes

Proceedings of the American Control Conference

Volumn 6, Issue , 2001, Pages 4357-4362

  Shtessel, Yuri B ^a   Hall, Charles E ^b  

^a UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

^b NASA MARSHALL SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE VEHICLES; AIRCRAFT ENGINES; CONTROL SYSTEM SYNTHESIS; DIFFERENTIAL EQUATIONS; EIGENVALUES AND EIGENFUNCTIONS; FAILURE (MECHANICAL); FLIGHT DYNAMICS; MATRIX ALGEBRA; ROBUSTNESS (CONTROL SYSTEMS);

MULTIPLE SCALE SLIDING MODE CONTROL; REUSABLE LAUNCH VEHICLE;

SLIDING MODE CONTROL;

EID: 0034840582     PISSN: 07431619     EISSN: None     Source Type: Journal    
DOI: 10.1109/ACC.2001.945663     Document Type: Article

References (9)

1. Variable structure PID control to prevent integral windup
2. Variable structure control of nonlinear multivariable systems: A tutorial
3. Reusable launch vehicle control in multiple time scale sliding modes
4. Sliding mode control of the X-33 vehicle in launch and re-entry modes
5. Invertibility and trajectory control for nonlinear manuevers of aircraft
6. Stability analysis of a continuous implementation of variable structure control