Prescribed performance control method for non-affine model of hypersonic vehicles

被引：1
|
作者：
Li X.-B. [1 ]
Zhao S.-Y. [2 ]
Bu X.-W. [1 ]
He Y.-G. [2 ]
机构：
[1] Air and Missile Defense College, Air Force Engineering University, Xi'an, 710051, Shaanxi
[2] Graduate College, Air Force Engineering University, Xi'an, 710051, Shaanxi
来源：
Kongzhi Lilun Yu Yingyong/Control Theory and Applications | 2019年 / 36卷 / 10期
关键词：
Hypersonic vehicles; Non-affine; Prescribed performance; Transient state; Virtual control law;
D O I：
10.7641/CTA.2019.80512
中图分类号：
学科分类号：
摘要：
Aiming at the non-affine model of hypersonic vehicle with high dynamic, fast time-varying, strong coupling, uncertainties and multi-constraints, a novel prescribed performance backstepping control method without estimation and approximation is designed. Firstly, the longitudinal model of hypersonic vehicle is decomposed into velocity subsystem and altitude subsystem, which are expressed as non-affine subsystems. Novel prescribed performance backstepping controllers are designed for the two subsystems respectively. The designed controller does not need the virtual control law to derive the time repeatedly, thus avoiding the "differential expansion problem". Secondly, the performance function is designed to ensure that the tracking error is limited to the expected range, so that the controller has satisfactory transient state and steady state performance, while significantly reducing the computational load. Finally, the effectiveness and feasibility of the controller are verified by simulation. © 2019, Editorial Department of Control Theory & Applications South China University of Technology. All right reserved.
引用
收藏
页码：1672 / 1681
页数：9
相关论文
共 31 条
  • [1] Sun C., Mu C., Yu Y., Some control problems for near space hypersonic vehicles, Acta Automatica Sinica, 39, 11, pp. 1901-1913, (2013)
  • [2] Bu X., Research progress in hypersonic vehicles control, Aviation Weapons, 1, pp. 47-61, (2018)
  • [3] Huang L., Duan Z., Yang J., The challenge to control science of near space hypersonic vehicles, Control Theory & Applications, 28, 10, pp. 1496-1505, (2011)
  • [4] Ouzts P., Soloway D., Moerder D., Et al., The role of guidance, navigation, and control in hypersonic vehicle multidisciplinary design and optimization, The 16th AIAA/DLR/DGLR International Space Planes & Hypersonic Systems & Technologies Conference, (2009)
  • [5] Sun C., Mu C., Zhang R., Terminal Sliding Mode Control Technology for Hypersonic Vehicle, (2014)
  • [6] An H., Liu J., Wu L., Disturbance observer-based anti-windup control for air-breathing hypersonic vehicles, IEEE Trans Ind Electron, 63, 5, pp. 3038-3049, (2016)
  • [7] Guo C., Liang X.G., Wang W.J., Et al., Mixed H<sub>2</sub>/H<sub>∞</sub> decentralized fuzzy tracking control design for a flexible air-breathing hypersonic vehicle, Proceedings of the Institution of Mechanical Engineers, Part I, 229, 5, pp. 388-405, (2015)
  • [8] Wu Y., Wang J., Liu X., Et al., Disturbance-observer-based sliding mode control for hypersonic flight vehicle, Control Theory & Applications, 32, 6, pp. 717-724, (2015)
  • [9] Wang J., Wu Y., Dong X., Sliding mode control for hypersonic flight vehicle with sliding mode disturbance observer, Acta Aeronautica et Astronautica Sinica, 36, 6, pp. 2027-2036, (2015)
  • [10] Dong Z., Lu Y., Wang Q., Command filtered backstepping control for hypersonic vehicles, Journal of Astronautics, 37, 8, pp. 957-963, (2016)
1234