DocumentCode
1730652
Title
Practical applications of modern controls for booster autopilot design
Author
Devirgilio, Miguel A. ; Kamimoto, Darren K.
Author_Institution
Aerosp. Corp., Los Angeles, CA, USA
fYear
1993
Firstpage
400
Lastpage
412
Abstract
This paper presents an evaluation of three of the most promising optimal control techniques for use in launch vehicle autopilot design. The methods evaluated are the EASY5 parameter optimizer, H∞, and SANDY/H2. Both the EASY5 parameter optimizer and SANDY/H2 are commercially available software packages based on constrained optimization. Recent advances in the application of H, control theory, such as response mode shaping (RMS), have made it a practical method for booster autopilot design. Three designs were successfully completed using a realistic booster model containing 16 bending modes. A summary is given for each method in terms of user friendliness and ability to meet design requirements. The EASY5 parameter optimization routine was the most user friendly and was considered to be an ideal tool for improving an existing design. Recent advances in the application of optimal control make H∞ and SANDY viable tools for booster autopilot design. SANDY was considered the best of the three booster autopilot design methods evaluated because of its flexibility to satisfy most of the design requirements, combined with a constrained parameter optimization
Keywords
aerospace computing; aircraft control; aircraft instrumentation; control system CAD; optimal control; optimisation; software packages; EASY5 parameter optimizer; SANDY/H2; avionics; bending modes; booster autopilot design; constrained optimization; constrained parameter optimization; control theory; design requirements; launch vehicle autopilot design; optimal control; optimization routine; realistic booster model; response mode shaping; software packages; user friendliness; Application software; Constraint optimization; Control theory; Design methodology; Design optimization; Human computer interaction; Optimal control; Optimization methods; Software packages; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1993. 12th DASC., AIAA/IEEE
Conference_Location
Fort Worth, TX
Print_ISBN
0-7803-1343-7
Type
conf
DOI
10.1109/DASC.1993.283516
Filename
283516
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