Reconfigurable inner loop control of a space maneuvering vehicle

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Oppenheimer, Michael W ^a   Doman, David B ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; CONTROL SURFACES; CONTROL THEORY; LAUNCHING; LINEAR PROGRAMMING; MANEUVERABILITY; REUSABILITY;

ALLOCATION SYSTEMS; ANGULAR ACCELERATION; DYNAMIC INVERSION; INNER LOOP CONTROLS; LINEAR ACCELERATIONS; LONGITUDINAL ACCELERATION; REUSABLE LAUNCH VEHICLES; SPACE MANEUVERING VEHICLES;

AUTOMOBILE BODIES;

EID: 85088343901     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5358     Document Type: Conference Paper

References (7)

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4. D. B. Doman and M. W. Oppenheimer, "Improving Control Allocation Accuracy for Nonlinear Aircraft Dynamics," in Proceedings of the 2002 Guidance, Navigation and Control Conference, AIAA 2002-4667, August 2002.
5. D. B. Doman and A. D. Ngo, "Dynamic inversion-based adaptive/reconfigurable control of the x-33 on ascent," Journal of Guidance, Control and Dynamics, vol. 25, no. 2, pp. 275-284, 2002.
6. B. Etkin, Dynamics of Atmospheric Flight. John Wiley & Sons, Inc., 1972.
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