Integrated missile guidance law and autopilot design using linear optimal control

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2000, Pages

  Hughes, Taylor L ^a   McFarland, Michael B ^b  

^a UNIVERSITY OF FLORIDA   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; ELECTRONIC GUIDANCE SYSTEMS; FEEDBACK LINEARIZATION; MANEUVERABILITY; NAVIGATION;

ATTITUDE STABILIZATION; INTEGRATED DESIGN APPROACHES; LINEAR APPROXIMATIONS; LINEAR OPTIMAL CONTROLS; MANEUVERING TARGETS; OPTIMAL CONTROL TECHNIQUE; OPTIMAL GUIDANCE LAW; PROPORTIONAL NAVIGATION;

GUIDED MISSILES;

EID: 85086489960     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4163     Document Type: Conference Paper

References (6)

1. Zarchan, P., Tactical and Strategic Missile Guidance, Washington, DC: AIAA Press, 1990.
2. Bryson, A. E., and Ho, Y.-C., Applied Optimal Control, New York: Hemisphere Publishing Corp., 1975.
3. Menon, P. K. A., et al., Integrated Control and Guidance Systems for High Angle of Attack Missiles, Final Report for USAF Wright Laboratory, Optimal Synthesis, Inc., Palo Alto, CA, 1995.
4. McFarland, M. B., Zachery, R. A., and Taylor, B. K., "Motion Planning for Reduced Observability of Autonomous Aerial Vehicles," Proceedings of the Conference on Control Applications, Hawaii, 1999.
5. Lin, C. F., et al., "Optimal Design of Integrated Missile Guidance and Control," Proceedings of the World Aviation Conference, Anaheim, CA, September, 1998.
6. Innocenti, A., and Thukral, A., "Simultaneous Reaction Jet and Aerodynamic Control of Missile Systems," Proceedings of the AIAA Guidance, Navigation, and Control Conference, 1993, pp. 347-354.