Missile longitudinal autopilots: Connections between optimal control and classical topologies

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

Volumn 7, Issue , 2005, Pages 5162-5190

  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; BANDWIDTH; OPTIMAL CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); TOPOLOGY;

CLASSICAL TOPOLOGIES; CONTROL ACTUATION SYSTEM (CAS); LOOP TOPOLOGY; MISSILE LONGITUDINAL AUTOPILOTS;

MISSILES;

EID: 29744465535     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-6381     Document Type: Conference Paper

References (4)

1. Paul Zarchan, Tactical and Strategic Missile Guidance. Fourth Edition, AIAA Volume 199 Progress in Astronautics and Aeronautics, Reston. VA, 2002
2. 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
3. C.P. Mracek and D.B. Ridgely, "Missile Longitudinal Autopilots: Comparison of Multiple Three Loop Topologies", AIAA GNC Conference. San Francisco CA, Aug. 2005
4. F.L. Lewis and V.L. Syrmos, "Optimal Control. Second Edition", John Wiley & Sons, Inc. New York, New York. 1995