Trajectory Tracking Control of Hypersonic Reentry Vehicle Based on Adaptive Fuzzy System

Article Preview

Abstract:

Considering inaccurate model and simplified calculation problems of the hypersonic reentry vehicle, this paper presents an adaptive fuzzy control system of the trajectory tracking control method. Firstly we introduced the principle of fuzzy system, then used fuzzy control theory to approximate the second-order drag acceleration model and got drag model by fuzzy identification, finally designed the adaptive controller. The simulation results show that the fuzzy adaptive tracking control method don’t depend on the dynamic model, but only rely on drag of the vehicle suffered, it can be measured directly or obtained by the aerodynamic model of the flight, the can generate tracking guidance control law, and the fuzzy adaptive tracking control method enables hypersonic vehicle to track the drag reference trajectory, realizes safe reentry and the terminal states can meet the requirements of the terminal constraints with high precision.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

378-384

Citation:

Online since:

November 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Z.J. Shen, P. Lu, Onboard generation of three-dimensional constrained entry trajectories, Journal of Guidance Control and Dynamics, Vol. 26, No. 1, Jan. 2003, pp.111-121.

DOI: 10.2514/2.5021

Google Scholar

[2] P. Lu, Entry guidance and trajectory control for reusable launch vehicle, Journal of Guidance Control and Dynamics, Vol. 20, No. 1, Jan. 1997, pp.143-149.

DOI: 10.2514/2.4008

Google Scholar

[3] J.A. Leavitt, A. Saraf, D.T. Chen, Performance of evolved acceleration guidance logic for entry(EAGLE), AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Press, Aug. 2002, pp.1-8.

DOI: 10.2514/6.2002-4456

Google Scholar

[4] Y.N. Hu, L.Q. Zhang, Fuzzy controller design theory and applications, China Machine Press, Beijing, 2010, pp.7-35.

Google Scholar

[5] C. Andrew, D. M. Maj, C. Wu and S. Choil, An Aero-Propulsion Integrated Elastic Model of a Generic Airbreathing Hypersonic Vehicle, AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Press, Aug. 2006, pp.154-173.

DOI: 10.2514/6.2006-6560

Google Scholar