一种舵面故障导弹控制分配优化方法
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摘要
该文研究了一种多操纵面导弹舵面故障情况下的控制分配优化设计方法,建立了相应的控制分配优化模型。针对由于多组基底效率相同产生的控制分配结果的跳变问题,基于基排序思想提出了一种基底选择方法。通过与传统分配方法的分配结果进行比较,验证了该文方法的有效性和灵活性。该文结果可为导弹的容错控制提供基础。
The control allocation optimization of the missile with multi-control effectors under the rudder fault condition is researched and the optimization model is established.A bases-choose method based on the bases sequence control allocation is given to overcome the mutation problem due to the same effectiveness of many bases.The comparation with the traditional allocation shows that the method in this paper has the good performance of accuracy and rapidity,and it can provide the foundation of the fault-tolerant control of missiles.
The control allocation optimization of the missile with multi-control effectors under the rudder fault condition is researched and the optimization model is established.A bases-choose method based on the bases sequence control allocation is given to overcome the mutation problem due to the same effectiveness of many bases.The comparation with the traditional allocation shows that the method in this paper has the good performance of accuracy and rapidity,and it can provide the foundation of the fault-tolerant control of missiles.
引文
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[2]杨恩泉,高金源.先进战斗机控制分配方法研究进展[J].飞行力学,2005,23(3):1-4.Yang Enquan,Gao Jinyuan.Research and development on advanced fighter control allocation methods[J].Flight Dynamics,2005,23(3):1-4.
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[7]王鹏,侯中喜,杨希祥.控制分配在平流层飞艇姿态控制中的应用[J].国防科技大学学报,2015,37(4):15-18.Wang Peng,Hou Zhongxi,Yang Xixiang.Control allocation approach for stratospheric airship attitude control[J].Journal of National University of Defense Technology,2015,37(4):15-18.
[8]史静平,章卫国,李广文,等.再分配伪逆算法分配效率研究[J].中国科学:信息科学,2010,40(4):519-525.Shi Jingping,Zhang Weiguo,Li Guangwen,et al.Research on allocation efficiency of the redistributed pseudo inverse algorithm[J].Science China Information Sciences,2010,40(4):519-525.
[9]曲小宇,章卫国,严谨,等.不动点法在飞控系统控制分配中的应用[J].计算机仿真,2009,26(9):66-69.Qu Xiaoyu,Zhang Weiguo,Yan Jin,et al.Application of fixed-point method in control allocation of flight control system[J].Computer Simulation,2009,26(9):66-69.
[10]池程芝,章卫国,高亚奎,等.基于改进不动点的多操纵面飞机重构控制分配[J].飞行力学,2012,30(6):515-518.Chi Chengzhi,Zhang Weiguo,Gao Yakui,et al.Reconfiguration control allocation of multi actuators aircraft based on improved fixed-point iteration[J].Flight Dynamics,2012,30(6):515-518.
[11]徐明兴.考虑非线性影响的飞翼布局无人机多舵面分配方法研究[D].西安:西北工业大学无人机特种技术重点实验室,2014.
[12]占正勇,刘林.多操纵面先进布局飞机控制分配技术研究[J].飞行力学,2006,24(1):13-16.Zhan Zhengyong,Liu Lin.Control allocation for high performance aircraft with multi-control effectors[J].Flight Dynamics,2006,24(1):13-16.
[13]朱心中,刘春生.基于控制分配的多操纵面战斗机重构控制研究及应用[J].东南大学学报(自然科学版),2010,40(s1):162-166.Zhu Xinzhong,Liu Chunsheng.Reconfigurable control based on control allocation for fighter with multiple effectors[J].Journal of Southeast University(Natural Science Edition),2010,40(s1):162-166.
[14]Harkegard O.Efficient active set algorithms for solving constrained least squares problems in aircraft control allocation[C]//Proceedings of the 42st IEEE Conference on the Decision and Control,2002.Las Vegas,US:IEEE,2003:1295-1300.
[15]曹宗涛,马瑞平,张明廉.一种飞行控制中控制分配的解决方案[J].飞行力学,2006,24(1):17-21.Cao Zongtao,Ma Ruiping,Zhang Minglian.A solution for aircraft control allocation[J].Flight Dynamics,2006,24(1):17-21.
[16]史静平,屈晓波,毕可军.一种基于转矩可达集的操纵面组合分配设计方法[J].西北工业大学学报,2014,32(1):123-130.Shi Jingping,Qu Xiaobo,Bi Kejun.A multiple effector control allocation method based on attainable moment subset[J].Journal of Northwestern Polytechnical University,2014,32(1):123-130.
[17]屈晓波.无尾飞翼飞机多操纵面控制分配技术研究[D].西安:西北工业大学自动化学院,2015.
[18]杨凌宇,高金源,申功璋.飞行控制中的一种新型最优控制分配方法[J].北京航空航天大学学报,2007,33(5):572-576.Yang Lingyu,Gao Jinyuan,Shen Gongzhang.New optimal control allocation method for flight control system[J].Journal of Beijing University of Aeronautics&Astronautics,2007,33(5):572-576.
[19]杨凌宇,范彦铭,邵山,等.基于基排序法的冗余操纵面控制分配与管理[J].中国科学(技术科学),2010(4):399-406.Yang Lingyu,Fan Yanming,Shao Shan,et al.Control allocation and management of redundant control effectors based on bases sequenced method[J].Sci China Tech Sci,2010(4):399-406.
[20]姜斌,杨浩.飞控系统主动容错控制技术综述[J].系统工程与电子技术,2007,29(12):2106-2110.Jiang Bin,Yang Hao.Survey of the active fault-tolerant control for flight control system[J].Systems Engineering&Electronics,2007,29(12):2106-2110.
[2]杨恩泉,高金源.先进战斗机控制分配方法研究进展[J].飞行力学,2005,23(3):1-4.Yang Enquan,Gao Jinyuan.Research and development on advanced fighter control allocation methods[J].Flight Dynamics,2005,23(3):1-4.
[3]马建军,李文强,李鹏,等.飞行器控制分配技术研究现状与展望[J].飞行力学,2009,27(3):1-5.Ma Jianjun,Li Wenqiang,Li Peng,et al.Status and future of control allocation for aerospace vehicle[J].Flight Dynamics,2009,27(3):1-5.
[4]Omerdic E.Thruster fault diagnosis and accommodation for overactuated open-frame underwater vehicles[D].Wales Newport,UK:Mechatronics Research Center,University of Wales Newport,2004.
[5]Bordignon K A.Constrained control allocation for systems with redundant control effectors[D].Virginia,US:Virginia Polytechnic Institute and State University,1996.
[6]Burken J J,Lu P,Wu Z,et al.Two reconfigurable flight-control design methods:Robust servomechanism and control allocation[J].Journal of Guidance Control&Dynamics,2001,24(3):482-493.
[7]王鹏,侯中喜,杨希祥.控制分配在平流层飞艇姿态控制中的应用[J].国防科技大学学报,2015,37(4):15-18.Wang Peng,Hou Zhongxi,Yang Xixiang.Control allocation approach for stratospheric airship attitude control[J].Journal of National University of Defense Technology,2015,37(4):15-18.
[8]史静平,章卫国,李广文,等.再分配伪逆算法分配效率研究[J].中国科学:信息科学,2010,40(4):519-525.Shi Jingping,Zhang Weiguo,Li Guangwen,et al.Research on allocation efficiency of the redistributed pseudo inverse algorithm[J].Science China Information Sciences,2010,40(4):519-525.
[9]曲小宇,章卫国,严谨,等.不动点法在飞控系统控制分配中的应用[J].计算机仿真,2009,26(9):66-69.Qu Xiaoyu,Zhang Weiguo,Yan Jin,et al.Application of fixed-point method in control allocation of flight control system[J].Computer Simulation,2009,26(9):66-69.
[10]池程芝,章卫国,高亚奎,等.基于改进不动点的多操纵面飞机重构控制分配[J].飞行力学,2012,30(6):515-518.Chi Chengzhi,Zhang Weiguo,Gao Yakui,et al.Reconfiguration control allocation of multi actuators aircraft based on improved fixed-point iteration[J].Flight Dynamics,2012,30(6):515-518.
[11]徐明兴.考虑非线性影响的飞翼布局无人机多舵面分配方法研究[D].西安:西北工业大学无人机特种技术重点实验室,2014.
[12]占正勇,刘林.多操纵面先进布局飞机控制分配技术研究[J].飞行力学,2006,24(1):13-16.Zhan Zhengyong,Liu Lin.Control allocation for high performance aircraft with multi-control effectors[J].Flight Dynamics,2006,24(1):13-16.
[13]朱心中,刘春生.基于控制分配的多操纵面战斗机重构控制研究及应用[J].东南大学学报(自然科学版),2010,40(s1):162-166.Zhu Xinzhong,Liu Chunsheng.Reconfigurable control based on control allocation for fighter with multiple effectors[J].Journal of Southeast University(Natural Science Edition),2010,40(s1):162-166.
[14]Harkegard O.Efficient active set algorithms for solving constrained least squares problems in aircraft control allocation[C]//Proceedings of the 42st IEEE Conference on the Decision and Control,2002.Las Vegas,US:IEEE,2003:1295-1300.
[15]曹宗涛,马瑞平,张明廉.一种飞行控制中控制分配的解决方案[J].飞行力学,2006,24(1):17-21.Cao Zongtao,Ma Ruiping,Zhang Minglian.A solution for aircraft control allocation[J].Flight Dynamics,2006,24(1):17-21.
[16]史静平,屈晓波,毕可军.一种基于转矩可达集的操纵面组合分配设计方法[J].西北工业大学学报,2014,32(1):123-130.Shi Jingping,Qu Xiaobo,Bi Kejun.A multiple effector control allocation method based on attainable moment subset[J].Journal of Northwestern Polytechnical University,2014,32(1):123-130.
[17]屈晓波.无尾飞翼飞机多操纵面控制分配技术研究[D].西安:西北工业大学自动化学院,2015.
[18]杨凌宇,高金源,申功璋.飞行控制中的一种新型最优控制分配方法[J].北京航空航天大学学报,2007,33(5):572-576.Yang Lingyu,Gao Jinyuan,Shen Gongzhang.New optimal control allocation method for flight control system[J].Journal of Beijing University of Aeronautics&Astronautics,2007,33(5):572-576.
[19]杨凌宇,范彦铭,邵山,等.基于基排序法的冗余操纵面控制分配与管理[J].中国科学(技术科学),2010(4):399-406.Yang Lingyu,Fan Yanming,Shao Shan,et al.Control allocation and management of redundant control effectors based on bases sequenced method[J].Sci China Tech Sci,2010(4):399-406.
[20]姜斌,杨浩.飞控系统主动容错控制技术综述[J].系统工程与电子技术,2007,29(12):2106-2110.Jiang Bin,Yang Hao.Survey of the active fault-tolerant control for flight control system[J].Systems Engineering&Electronics,2007,29(12):2106-2110.