DocumentCode :
1600803
Title :
Automated gain schedules for missile autopilots using robustness theory
Author :
Eberhardt, Rowena ; Wise, Kevin A.
Author_Institution :
McDonnell Douglas Missile Syst. Co., St. Louis, MO, USA
fYear :
1992
Firstpage :
243
Abstract :
Preliminary results in computer-automated missile flight control design are presented. The structured singular value μ is used to automate the calculation of gain schedules for a missile autopilot. Using μ-analysis, the approach guarantees both stability and performance robustness between the gain scheduled grid points
Keywords :
aerospace computer control; control system CAD; missiles; stability; μ-analysis; computer-automated missile flight control design; gain schedules; missile autopilots; performance robustness; stability; structured singular value; Aerospace control; Job shop scheduling; Missiles; Performance gain; Processor scheduling; Robust control; Robust stability; Robustness; Testing; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 1992., First IEEE Conference on
Conference_Location :
Dayton, OH
Print_ISBN :
0-7803-0047-5
Type :
conf
DOI :
10.1109/CCA.1992.269869
Filename :
269869
Link To Document :
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