Research on Parameter Optimization Method of an Air Vehicle Gliding Trajectory

Fang Peng Wang; Yong Xu; Chun Ying Li

doi:10.4028/www.scientific.net/AMR.945-949.662

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 945-949Research on Parameter Optimization Method of an...

Research on Parameter Optimization Method of an Air Vehicle Gliding Trajectory

Abstract:

A mathematical model of air vehicle gliding trajectory was established and attack angle was regarded as control variable. Adaptive simulated annealing algorithm was adopted to optimize the 101 nodes of attack angle. By optimizing the control law of attack angle of gliding trajectory, the maximum range of air vehicle is increased significantly, which increases 107%.

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Periodical:

Advanced Materials Research (Volumes 945-949)

Pages:

662-665

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.945-949.662

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Online since:

June 2014

Authors:

Fang Peng Wang, Yong Xu*, Chun Ying Li

Keywords:

Adaptive Simulated Annealing Algorithm, Air Vehicle, Parameter Optimization, Trajectory

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* - Corresponding Author

References

[1] E. M. Yong, G. J. Tang, L. Chen. Numerical Method Review for the Trajectory Optimization of Air Vehicle. Journal of Astronautics, 2008，29(2): 398-406.

Google Scholar

[2] X. F. Qian, R. X. Lin, Y. N. Zhao, in: Missile Flight Aerodynamics, Beijing Institute of Technology Press, 2000. ( in Chinese ).

Google Scholar

[3] P. R. Jia, K. J. Chen, L. He, in: Ballistic for Long Range Rocket, National University of Defense Technology Press, 1993: 40- 42. ( in Chinese ).

Google Scholar

[4] L. J. Ding, in: Numerical Calculation Method, Beijing Institute of Technology Press, 2000. ( in Chinese ).

Google Scholar

[5] LESTER I. Adaptive Simulated Annealing(ASA): lessons learned[J]. Control and Cybernetics Journal, 1996, 25: 33-54.

Google Scholar

[6] LESTER I. Very Fast Simulated Reannealing [J]. Mathematical Computer Modeling, 1989(12): 967-973.

Google Scholar