Gain scheduled missile autopilot design using a control signal interpolation technique

1998 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1998, Pages 1394-1402

  Lawrence, Douglas A ^a   Kelly, Joy H ^b   Evers, Johnny H ^b  

^a OHIO UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; FLIGHT SIMULATORS; INTERPOLATION; MISSILES;

CONTROL SIGNAL; INTERPOLATION SCHEMES; MISSILE AUTOPILOT; MISSILE AUTOPILOT DESIGN; NONLINEAR GAINS; NONLINEAR SIMULATIONS; PITCH CHANNELS; POINT DESIGN;

CONTROL SYSTEM SYNTHESIS;

EID: 46449121303     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4418     Document Type: Conference Paper

References (8)

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3. J. H. Kelly and J. H. Evers, "An Interpolation Strategy for Scheduling Dynamic Compensators", Proceedings of the 1997 AIAA Guidance, Navigation and Control Conference, New Orleans, Louisiana, 1997.
4. D. A. Lawrence, "Tools for the Analysis and Design of Gain Scheduled Missile Autopilots", Final Report, 1997 AFOSR Summer Research Extension Program, December, 1997.
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7. C. P. Mracek and J. R. Cloutier, "Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method", Proceedings of the 1997 AIAA Guidance, Navigation and Control Conference, New Orleans, Louisiana, 1997.
8. R. A. Nichols, R. T. Reichert, and W. J. Rugh, "Gain Scheduling for H-Infinity Controllers: A Flight Control Example", IEEE Transactions on Control Systems Technology, Vol. 1, No. 2, pp. 69-79, 1993.