Gain-scheduled missile autopilot design using linear parameter varying transformations

Journal of Guidance, Control, and Dynamics

Volumn 16, Issue 2, 1993, Pages 256-263

  Shamma, Jeff S ^a,c   Cloutier, James R ^b,d  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Department of Aerospace Engineering and Engineering Mechanics ^*  (United States)

^d Wright Laboratory WL/MNAG ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEMS; FLIGHT DYNAMICS; MATHEMATICAL TRANSFORMATIONS;

AUTOPILOTS; GAIN SCHEDULED DESIGN; LINEAR PARAMETER VARYING;

MISSILES;

EID: 0027559799     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.20997     Document Type: Article

References (11)

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3. Balas, G., Doyle, J. C., Glover, K., Packard, A., and Smith, R., “i-Analysis and Synthesis Toolbox: -Tools,” MUSYN, Inc., and The Mathworks, Inc., Dec. 1990.
4. Isidori, A., Nonlinear Control Systems: An Introduction, Vol. 72, Lecture Notes in Control and Information Science, Springer-Verlag, Berlin, 1985.
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9. Shahruz, S. M., and Behtash, S., “Design of Controllers for Linear Parameter Varying Systems by the Gain Scheduling Technique,” Berkeley Engineering Research Inst., Memorandum BERI M90/1, Univ. of California, Berkeley, CA, Jan. 1990.
10. Shamma, J. S., and Athans, M., “Gain Scheduling: Potential Hazards and Possible Remedies,” IEEE Control Systems Magazine, June 1992.
11. Desoer, C. A., and Vidyasagar, M., Feedback Systems: Input-Output Properties, Academic, New York, 1975.