Adaptive Multivariable Finite-Time Reentry Attitude Control for RLV
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- 英文论文题名：Adaptive Multivariable Finite-Time Reentry Attitude Control for RLV
- 论文作者：Bailing Tian ; Yuxin Ma ; Yunpeng Zhang ; Qun Zong
- 英文论文作者：Bailing Tian ; Yuxin Ma ; Yunpeng Zhang ; Qun Zong ; School of Electrical and Information Engineering ; Tianjin University ; Science and Technology on Aircraft Control Laboratory ; FACRI
- 年：2017
- 作者机构：School of Electrical and Information Engineering,Tianjin University;Science and Technology on Aircraft Control Laboratory,FACRI;
- 英文论文关键词：Adaptive multivariable controller ; finite-time convergence ; reusable launch vehicle(RLV)
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（A）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
- 语种：英文
- 分类号：V448
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：5
- 文件大小：370k
- 原文格式：D
- 会议级别：全国
摘要
The finite-time tracking control for reusable launch vehicle with matched disturbance is investigated. An adaptivemultivariable controller is proposed where the bounds of the perturbations are not known. A proof of the finite-time convergence of the closed-loop system is derived using the Lyapunov technique. The feature of the proposed control scheme is that it does not require any information on the bounds of the disturbance and its gradient except for their existence. Finally, some simulation tests are provided to demonstrate the effectiveness of the proposed control scheme.
The finite-time tracking control for reusable launch vehicle with matched disturbance is investigated. An adaptivemultivariable controller is proposed where the bounds of the perturbations are not known. A proof of the finite-time convergence of the closed-loop system is derived using the Lyapunov technique. The feature of the proposed control scheme is that it does not require any information on the bounds of the disturbance and its gradient except for their existence. Finally, some simulation tests are provided to demonstrate the effectiveness of the proposed control scheme.
The finite-time tracking control for reusable launch vehicle with matched disturbance is investigated. An adaptivemultivariable controller is proposed where the bounds of the perturbations are not known. A proof of the finite-time convergence of the closed-loop system is derived using the Lyapunov technique. The feature of the proposed control scheme is that it does not require any information on the bounds of the disturbance and its gradient except for their existence. Finally, some simulation tests are provided to demonstrate the effectiveness of the proposed control scheme.
引文
[1]Skariya S E,Sebastian B,Namboodiripad M N.Integrated Optimal Control of Reusable launch Vehicle and Actuation system using Linear Quadratic Regulator[J].IFAC Proceedings Volumes,2014,47(1):840-846.
[2]Li A,Yang L,Zhang J,et al.LQR and Fuzzy Gain-Scheduling based attitude controller for RLV within large operating envelope[C]//IEEE International Conference on Control Science and Systems Engineering.IEEE,2014:51-56.
[3]M.Xin,Y.J.Xu,and P.Vedula,Nonlinear stochastic control part II:Ascent phase control for reusable vehicles,presented at the AIAA Guidance,Navigation,Control Conference,Chicago,IL,USA,Aug.2009,Paper AIAA-2009-5956.
[4]Sun C Z,Huang Y M,Guo S F.Reusable launch vehicle pitch attitude control system research by trajectory linearization[J].Journal of Aerospace Power,2008,23(10):1921-1926.
[5]Lam Q,Krishnamurthy P,Khorrami F.Enhancing Flight Control System Performance Using SDRE Based Controller as an Augmentation Layer[C]//AIAA Guidance,Navigation,and Control Conference.2013.
[6]Q.M.Lam and M.Xin,Robustness evaluation of Theta-D technique for spacecraft attitude control subject to reaction wheel failures,presented at the AIAA Guidance,Navigation,Control Conference,Toronto,ON,Canada,Aug.2010,Paper AIAA-2010-8302.
[7]Qu S,Xia X,Zhang J.Dynamics of Discrete-Time SlidingMode-Control Uncertain Systems With a Disturbance Compensator[J].IEEE Transactions on Industrial Electronics,2014,61(7):3502-3510.
[8]Hall C,Shtessel Y.RLV Sliding Mode Control System Using Sliding Mode Observers and Gain Adaptation[C]//AIAA Guidance,Navigation,and Control Conference and Exhibit.2013.
[9]Tian B,Yin L,Wang H.Finite-Time Reentry Attitude Control Based on Adaptive Multivariable Disturbance Compensation[J].IEEE Transactions on Industrial Electronics,2015,62(9):5889-5898.
[10]Basin M and Ramirez P.A supertwisting algorithm for systems of dimension more than one[J].IEEE Transaction on Industrial Electronics,2014,61(11):6472-6480.
[11]Tian B,Zong Q.Optimal guidance for reentry vehicles based on indirect Legendre pseudospectral method[J].Acta Astronautica,2011,68(7-8):1176-1184.
[2]Li A,Yang L,Zhang J,et al.LQR and Fuzzy Gain-Scheduling based attitude controller for RLV within large operating envelope[C]//IEEE International Conference on Control Science and Systems Engineering.IEEE,2014:51-56.
[3]M.Xin,Y.J.Xu,and P.Vedula,Nonlinear stochastic control part II:Ascent phase control for reusable vehicles,presented at the AIAA Guidance,Navigation,Control Conference,Chicago,IL,USA,Aug.2009,Paper AIAA-2009-5956.
[4]Sun C Z,Huang Y M,Guo S F.Reusable launch vehicle pitch attitude control system research by trajectory linearization[J].Journal of Aerospace Power,2008,23(10):1921-1926.
[5]Lam Q,Krishnamurthy P,Khorrami F.Enhancing Flight Control System Performance Using SDRE Based Controller as an Augmentation Layer[C]//AIAA Guidance,Navigation,and Control Conference.2013.
[6]Q.M.Lam and M.Xin,Robustness evaluation of Theta-D technique for spacecraft attitude control subject to reaction wheel failures,presented at the AIAA Guidance,Navigation,Control Conference,Toronto,ON,Canada,Aug.2010,Paper AIAA-2010-8302.
[7]Qu S,Xia X,Zhang J.Dynamics of Discrete-Time SlidingMode-Control Uncertain Systems With a Disturbance Compensator[J].IEEE Transactions on Industrial Electronics,2014,61(7):3502-3510.
[8]Hall C,Shtessel Y.RLV Sliding Mode Control System Using Sliding Mode Observers and Gain Adaptation[C]//AIAA Guidance,Navigation,and Control Conference and Exhibit.2013.
[9]Tian B,Yin L,Wang H.Finite-Time Reentry Attitude Control Based on Adaptive Multivariable Disturbance Compensation[J].IEEE Transactions on Industrial Electronics,2015,62(9):5889-5898.
[10]Basin M and Ramirez P.A supertwisting algorithm for systems of dimension more than one[J].IEEE Transaction on Industrial Electronics,2014,61(11):6472-6480.
[11]Tian B,Zong Q.Optimal guidance for reentry vehicles based on indirect Legendre pseudospectral method[J].Acta Astronautica,2011,68(7-8):1176-1184.