Control allocation for the X-35B

2002 Biennial International Powered Lift Conference and Exhibit

Volumn , Issue , 2002, Pages

  Bordignon, Ken ^a   Bessolo, John ^a  

^a LOCKHEED MARTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

INVERSE PROBLEMS; LIFT; OUTAGES; SUPERSONIC AIRCRAFT;

CONTROL ALLOCATION; CONTROL EFFECTIVENESS; ENGINE POWER SETTINGS; GENERALIZED INVERSE; JOINT STRIKE FIGHTERS; PERFORMANCE REQUIREMENTS; SHORT TAKE-OFF AND VERTICAL LANDINGS; STRUCTURAL COUPLING;

RESEARCH AIRCRAFT;

EID: 85068894835     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-6020     Document Type: Conference Paper

References (4)

1. Brinker, J.S., Wise, K.A., "Stability and Flying Qualities Robustness of a Dynamic Inversion Aircraft Control Law", Journal of Guidance, Control, and Dynamics, Vol. 19, No. 6, 1996, pp.1270-1277
2. Enns, D., Bugajski, D., Hendrick, R., and Stein, G., "Dynamic Inversion: An Evolving Methodology for Flight Control Design", Flight Mechanic Symposium, Turin Italy, May 1994
3. Honeywell & Lockheed, Martin, "Multivariable Control Design Guidelines," Final Report to U.S.A.F. Program on Application of Multivariable Control Theory to Aircraft Control Laws, WL-TR-3099, August, 1996
4. Bordignon, K., "Constrained Control Allocation for Systems with Redundant Control Effectors", Ph.D. Dissertation, Virginia Polytechnic Institute & State University, 1996