DocumentCode :
2269854
Title :
Optimization based parameter identification of the Caltech ducted fan
Author :
Franz, Ryan ; Hauser, John
Author_Institution :
Northrop Grumman Space Technol., Redondo Beach, CA, USA
Volume :
3
fYear :
2003
fDate :
4-6 June 2003
Firstpage :
2697
Abstract :
Recent work has demonstrated the use of model predictive control (MPC) for stabilizing the Caltech ducted fan. In results published up until now, however, additional stability augmentation was required. It was felt that an inadequate model was the cause of this shortcoming. This paper details an optimization-based parameter identification scheme which was used to identify new parameters for the ducted fan model. In addition to solving a traditional least squares optimization problem over the space of parameters, we introduce the additional concept of optimizing over the space of inputs as in a typical optimal control problem. The projection operator approach to trajectory optimization described is used to perform the trajectory optimization and enables many iterations to be executed in a reasonable time span. Finally, the newly identified parameters enabled us to use pure MPC with no additional stability augmentation. We were unable to achieve the same results consistently with other techniques.
Keywords :
iterative methods; least squares approximations; nonlinear systems; optimal control; optimisation; parameter estimation; predictive control; wind tunnels; Caltech ducted fan; least squares optimization; model predictive control; optimal control; parameter identification; projection operator approach; stability; trajectory optimization; Aerodynamics; Least squares methods; Nonlinear systems; Optimal control; Optimization methods; Parameter estimation; Space technology; Stability; Unmanned aerial vehicles; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2003. Proceedings of the 2003
ISSN :
0743-1619
Print_ISBN :
0-7803-7896-2
Type :
conf
DOI :
10.1109/ACC.2003.1243486
Filename :
1243486
Link To Document :
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