Robust Attitude Control for Reusable Launch Vehicles Based on Fractional Calculus and Pigeon-inspired Optimization

Qiang Xue; Haibin Duan

Volume 4 Issue 1

Jan. 2017

IEEE/CAA Journal of Automatica Sinica

JCR Impact Factor: 15.3, Top 1 (SCI Q1)

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Article Navigation > IEEE/CAA Journal of Automatica Sinica > 2017 > 4(1): 89-97

Qiang Xue and Haibin Duan, "Robust Attitude Control for Reusable Launch Vehicles Based on Fractional Calculus and Pigeon-inspired Optimization," IEEE/CAA J. Autom. Sinica, vol. 4, no. 1, pp. 89-97, Jan. 2017.

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Qiang Xue and Haibin Duan, "Robust Attitude Control for Reusable Launch Vehicles Based on Fractional Calculus and Pigeon-inspired Optimization," IEEE/CAA J. Autom. Sinica, vol. 4, no. 1, pp. 89-97, Jan. 2017.

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Robust Attitude Control for Reusable Launch Vehicles Based on Fractional Calculus and Pigeon-inspired Optimization

Bio-inspired Autonomous Flight Systems (BAFS) Research Group, the Science and Technology on Aircraft Control Laboratory, School of Automation Science and Electrical Engineering, Beihang University (BUAA), Beijing 100083, China

Funds:

National Natural Science Foundation of China 61425008

National Natural Science Foundation of China 61333004

National Natural Science Foundation of China 61273054

Top-Notch Young Talents Program of China, and Aeronautical Foundation of China 2015ZA51013

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Abstract

Abstract

In this paper, a robust attitude control system based on fractional order sliding mode control and dynamic inversion approach is presented for the reusable launch vehicle (RLV) during the reentry phase. By introducing the fractional order sliding surface to replace the integer order one, we design robust outer loop controller to compensate the error introduced by inner loop controller designed by dynamic inversion approach. To take the uncertainties of aerodynamic parameters into account, stochastic robustness design approach based on the Monte Carlo simulation and Pigeon-inspired optimization is established to increase the robustness of the controller. Some simulation results are given out which indicate the reliability and effectiveness of the attitude control system.
- Attitude control,
- fractional calculus,
- pigeoninspired optimization,
- reusable launch vehicle (RLV),
- sliding mode control

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References(23)

References

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Robust Attitude Control for Reusable Launch Vehicles Based on Fractional Calculus and Pigeon-inspired Optimization

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