Missile longitudinal autopilots: Comparison of multiple three loop topologies

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 7, Issue , 2005, Pages 5134-5161

  Mracek, Curtis P ^a,b   Ridgely, D Brett ^a,b  

^a RAYTHEON COMPANY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION CONTROL; ACTUATORS; ERROR ANALYSIS; OPTIMAL CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); TOPOLOGY;

ACCELERATION ERRORS; CONTROL DEFLECTION; EQUIVALENT CLOSED LOOP PROPERTIES; MISSILE LONGITUDINAL AUTOPILOTS;

MISSILES;

EID: 29744462418     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-6380     Document Type: Conference Paper

References (5)

1. C.P. Mracek and D.B. Ridgely, "Missile Longitudinal Autopilots: Connections Between Optimal Control and Classical Topologies". GNC Conference, San Francisco, CA, Aug. 2005
2. Paul Zarchan, Tactical and Strategic Missile Guidance, Fourth Edition. AIAA Volume 109 Progress in Astronautics and Aeronautics, Reston, VA, 2002
3. I. Ashkenas, D. McGruer and D. Graham, Aircraft Dynamics and Automatic Control. Princeton University Press, 1973.
4. F.L. Lewis and V.L. Syrmos, "Optimal Control, Second Edition", John Wiley & Sons, Inc. New York, New York, 1995
5. R. J. Adams and N.M. Conrardy. "Design Plant Manipulations for Implementation of an LQR Controller in a Classical Three Loop Autopilot." Technical report, Raytheon Missile Systems, Apr. 2003