Model predictive control design for XV-15 tilt rotor flight control

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Mehra, R K ^a   Prasanth, R K ^a   Bennett, R L ^b   Neckels, D ^b   Wasikowski, M ^b  

^a SCIENTIFIC SYSTEMS COMPANY INC   (United States)

^b BELL HELICOPTER TEXTRON INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; FLIGHT CONTROL SYSTEMS; FLIGHT SIMULATORS; OPTIMIZATION; PREDICTIVE CONTROL SYSTEMS;

AUGMENTATION SYSTEMS; LINEAR PARAMETER VARYING; MODEL PREDICTIVE CONTROLLERS; OPTIMIZATION PROBLEMS; REAL TIME SIMULATORS; REAL-TIME APPLICATION; SOLUTION TECHNIQUES; STABILITY AND CONTROL;

MODEL PREDICTIVE CONTROL;

EID: 85087187980     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-4331     Document Type: Conference Paper

References (5)

1. M. Kothare et al., "Robust constrained model predictive control using linear matrix inequalities", Automatica, Vol. 32, No. 10, 1996.
2. D. Q. Mayne et al., "Constrained model predictive control: stability and optimality", Automatica, Vol.36, No.6, 2000.
3. A. Packard, "Gain scheduling via linear fractional transformations", Sys. Cont. Lett, Vol. 22, 1994.
4. J. Shamma and M. Athans, "Guaranteed properties of gain scheduled control for linear parameter varying plants", Automatica, Vol. 27, pp. 559-564, 1991.
5. J. Shamma and J. R. Cloutier, "A linear parameter varying approach to gain scheduled missile autopilot design", Proc. ACC, 1992, pp. 1317-1321.