DocumentCode
2387884
Title
Adaptive control and the NASA X-15 program: A concise history, lessons learned, and a provably correct design
Author
Dydek, Zachary T. ; Annaswamy, Anuradha M. ; Lavretsky, Eugene
Author_Institution
Dept. of Mech. Eng., Massachusetts Inst. of Technol., Cambridge, MA
fYear
2008
fDate
11-13 June 2008
Firstpage
2957
Lastpage
2962
Abstract
The NASA X-15 research airplane was one of the earliest aircraft to feature an adaptive control scheme, making its first flight in 1959. The program is largely considered a success, the one exception being the fatal accident that occurred on November 15, 1967. The circumstances which led to the anomalous behavior of the X-15 during that flight are reproduced using a fully nonlinear six-degree-of-freedom aircraft model and a detailed model of the original MH-96 adaptive controller. Using the lessons learned from the X-15 program as well as decades of work in the field of stable adaptive control, a provably correct (PC) adaptive controller is designed for the X-15. When subjected to the same conditions that caused the original MH-96 adaptive controller to fail, the PC adaptive controller is able to recover and complete the maneuver successfully.
Keywords
adaptive control; aircraft control; control system synthesis; history; nonlinear control systems; MH-96 adaptive controller; NASA X-15 research airplane; nonlinear six-degree-of-freedom aircraft model; provably correct adaptive controller; stable adaptive control; Accidents; Adaptive control; Aerodynamics; Aerospace control; Aircraft; History; Low earth orbit satellites; NASA; Programmable control; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2008
Conference_Location
Seattle, WA
ISSN
0743-1619
Print_ISBN
978-1-4244-2078-0
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2008.4586945
Filename
4586945
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