一套完整的基于视觉光流和激光扫描测距的室内无人机导航系统

王飞; 崔金强; 陈本美; 李崇兴

doi:10.3724/SP.J.1004.2013.01889

一套完整的基于视觉光流和激光扫描测距的室内无人机导航系统

doi: 10.3724/SP.J.1004.2013.01889

1.
新加坡国立大学综合科学与工程研究生院新加坡 119077;
2.
新加坡国立大学电气和计算机工程系新加坡 119077

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出版历程
- 收稿日期: 2013-07-10
- 修回日期: 2013-08-29
- 刊出日期: 2013-11-20

A Comprehensive UAV Indoor Navigation System Based on Vision Optical Flow and Laser FastSLAM

1.
Graduate School for Integrative Sciences and Engineering, Na-tional University of Singapore (NUS), Singapore, Singapore;
2.
De-partment of Electrical and Computer Engineering, National Univer-sity of Singapore, Singapore, Singapore

More Information

Corresponding author: CHEN Ben-Mei

摘要

摘要: 提出了一套室内四旋翼无人机控制, 导航, 定位和地图构建的完整解决方案. 无人机机载系统包括三个主要传感器, 即惯性测量单元, 下视相机和激光扫描测距仪. 经过处理, 融合这些传感器的测量数据, 无人机能够可靠的估计自己的飞行速度和实时位置, 并且沿着室内的墙壁进行无碰撞飞行. 通过收集一个完整飞行实验的数据, 无人机的飞行路径和在室内的环境也可以被很好地估计出来. 这套系统中的自主导功能不需要任何远程传感信息或脱机计算能力. 这套室内导航方案的性能和可靠性已在实际的飞行实验中被验证.
- 无人机飞行控制 /
- 室内导航 /
- 同步定位与地图构建
Abstract: This paper presents a comprehensive control, navigation, localization and mapping solution for an indoor quadrotor unmanned aerial vehicle (UAV) system. Three main sensors are used onboard the quadrotor platform, namely an inertial measurement unit, a downward-looking camera and a scanning laser rangefnder. With this setup, the UAV is able to estimate its own velocity and position robustly, while fying along the internal walls of a room without collisions. After one complete fight, with the collected data the historic UAV path and the indoor environment can be well estimated. The autonomous navigation part of the system does not require any remote sensory information or off-line computational power, while the mapping is done off-line. Complete fight tests have been carried out to verifyfdelity and performance the navigation solution.
- Unmanned aerial vehicle (UAV) fight control /
- indoor navigation /
- simultaneous localization and mapping (SLAM)

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参考文献(116)

[1]	Huang Lin, Duan Zhi-Sheng, Yang Ying. Several problems on control of modern aerocraft. Science and Technology Review, 2008, 26(20): 92-98 (黄琳, 段志生, 杨莹. 现代飞行器控制的几个科学问题. 科技导报, 2008, 26(20): 92-98)
[2]	Cui Er-Jie. Research statutes, development trends and key technical problems of near space flying vehicles. Advances in Mechanics, 2009, 39(6): 658-673 (崔尔杰. 近空间飞行器研究发展现状及关键技术问题. 力学进展, 2009, 39(6): 658-673)
[3]	Clark A, Wu C, Mirmirani M, Choi S B. Development of an airframe-propulsion integrated hypersonic vehicle model. In: Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada: American Institute of Aeronautics and Astronautics, 2006. AIAA 2006-218
[4]	Zhang Jing-Nan, Sun Wei-Meng, Zheng Zhi-Qiang. Discussion of control technique of hypersonic weapon. Aero Weaponry, 2006, (4): 11-13 (张静男, 孙未蒙, 郑志强. 高超声速武器控制技术发展探讨. 航空兵器, 2006, (4): 11-13)
[5]	Fidan B, Mirmirani M, Ioannou P A. Flight dynamics and control of air-breathing hypersonic vehicles: review and new directions. In: Proceedings of the 12th AIAA International Space Planes and Hypersonic Systems and Technologies. Norfolk, Virginia: American Institute of Aeronautics and Astronautics, 2003. AIAA 2003-7081
[6]	Yong En-Mi, Tang Guo-Jin, Chen Lei. Rapid trajectory planning for hypersonic unpowered long-range reentry vehicles with multi-constraints. Journal of Astronautics, 2008, 29(1): 46-52 (雍恩米, 唐国金, 陈磊. 高超声速无动力远程滑翔飞行器多约束条件下的轨迹快速生成. 宇航学报, 2008, 29(1): 46-52)
[7]	Wei Jian-Li, Yu Yun-Feng, Yan Jie. Research on robust control of hypersonic vehicle. Journal of Astronautics, 2008, 29(5): 1526-1530 (尉建利, 于云峰, 闫杰. 高超声速飞行器鲁棒控制方法研究. 宇航学报, 2008, 29(5): 1526-1530)
[8]	Bolender M A, Doman D B. Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle. Journal of Spacecraft and Rockets, 2007, 44(2): 374-387
[9]	Shaughnessy J D, Pinckney S Z, McMinn J D, Cruz C I, Kelley M L. Hypersonic Vehicle Simulation Model: Winged-Cone Configuration. NASA Technical Memorandum 102610, NASA Langley Research Center, USA, 1990
[10]	Heller M, Sachs G, Gunnarsson K S, Frank H, Rylander D. Flight dynamics and robust control of a hypersonic test vehicle with ramjet propulsion. In: Proceedings of the 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 1998. AIAA 1998-1521
[11]	Keshmiri S, Colgren R, Mirmirani M. Development of an aerodynamic database for a generic hypersonic air vehicle. In: Proceedings of the 2005 AIAA Guidance, Navigation, and Control Conference and Exhibit. San Francisco, California: American Institute of Aeronautics and Astronautics, 2005. AIAA 2005-6257
[12]	Colgren R, Keshmiri S, Mirmirani M. Nonlinear ten-degree-of-freedom dynamics model of a generic hypersonic vehicle. Journal of Aircraft, 2009, 46(3): 800-813
[13]	Lee J. Modeling and Controller Design for Hypersonic Vehicles [Ph.D. dissertation], University of Kansas, USA, 2006
[14]	Huo Y, Mirmirani M, Ioannou P, Kuipers M. Altitude and velocity tracking control for an airbreathing hypersonic cruise vehicle. In: Proceedings of the 2006 AIAA Guidance, Navigation, and Control Conference and Exhibit. Keystone, Colorado: American Institute of Aeronautics and Astronautics, 2006. AIAA 2006-6695
[15]	Kuipers M, Mirmirani M, Ioannou P, Huo Y. Adaptive control of an aeroelastic airbreathing hypersonic cruise vehicle. In: Proceedings of the 2007 AIAA Guidance, Navigation and Control Conference and EXhibit. Hilton Head, South California: American Institute of Aeronautics and Astronautics, 2007. AIAA 2007-6326
[16]	Kuipers M, Ioannou P, Fidan B. Robust adaptive multiple model controller design for an airbreathing hypersonic vehicle model. In: Proceedings of the 2008 AIAA Guidance, Navigation and Control Conference and Exhibit. Honolulu, Hawaii: American Institute of Aeronautics and Astronautics, 2008. AIAA 2008-7142
[17]	Chavez F R, Schmidt D K. Analytical aeropropulsive-aeroelastic hypersonic-vehicle model with dynamic analysis. Journal of Guidance, Control, and Dynamics, 1994, 17(6): 1308-1319
[18]	Williams T, Bolender M A, Doman D B, Morataya O. An aerothermal flexible mode analysis of a hypersonic vehicle. In: Proceedings of the 2006 AIAA Atmospheric Flight Mechanics Conference and Exhibit. Keystone, Colorado: American Institute of Aeronautics and Astronautics, 2006. AIAA 2006-6647
[19]	Parker J T, Serrani A, Yurkovich S, Bolender M A, Doman D B. Control-oriented modeling of an air-breathing hypersonic vehicle. Journal of Guidance, Control, and Dynamics, 2007, 30(3): 856-869
[20]	Yao Z H, Bao W, Chang J, Yu D, Tang J. Modelling for couplings of an airframe-propulsion integrated hypersonic vehicle with engine safety boundaries. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2010, 224(1): 43-55
[21]	Keshmiri S, Colgren R, Mirmirani M. Six-DOF modeling and simulation of a generic hypersonic vehicle for control and navigation purposes. In: Proceedings of the 2006 AIAA Guidance, Navigation, and Control Conference and Exhibit. Keystone, Colorado: American Institute of Aeronautics and Astronautics, 2006. AIAA 2006-6694
[22]	Zhang Jun, Jiang Chang-Sheng, Fang Wei. Variable structure near space vehicle control characteristics of large flight envelope. Journal of Astronautics, 2009, 30(2): 543-549 (张军, 姜长生, 方炜. 变结构近空间飞行器大飞行包络控制特性研究. 宇航学报, 2009, 30(2): 543-549)
[23]	Qian Cheng-Shan. Robust Control for Aerospace Vehicles Based on Multi-model [Ph.D. dissertation], Nanjing University of Aeronautics and Astronautics, China, 2008 (钱承山. 空天飞行器多模型鲁棒控制研究 [博士学位论文], 南京航空航天大学, 中国, 2008)
[24]	Brockhaus R. Flight Control. Beijing: National Defence Industry Press, 1999 (布罗克豪斯. 飞行控制. 北京: 国防工业出版社, 1999)
[25]	Guo Suo-Feng, Shen Gong-Zhang, Wu Cheng-Fu. Advanced Flight Control System. Beijing: National Defence Industry Press, 2003 (郭锁凤, 申功璋, 吴成福. 先进飞行控制系统. 北京: 国防工业出版社, 2003)
[26]	Marrison C I, Stengel R F. Design of robust control systems for a hypersonic aircraft. Journal of Guidance, Control, and Dynamics, 1998, 21(1): 58-63
[27]	Naidu S D, Banda S S, Bufington J L. Unified approach to H2 and H_{∞ optimal control of a hypersonic vehicle. In: Proceedings of the 1999 American Control Conference. San Diego, California: IEEE, 1999. 2737-2741
[28]	Gao H J, Si Y L, Li H Y, Hu X X, Wang C H. Modeling and control of an air-breathing hypersonic vehicle. In: Proceedings of the 7th Asian Control Conference. Hong Kong, China: IEEE, 2009. 304-307
[29]	Lei Y, Cao C Y, Cliff E, Hovakimyan N, Kurdila A, Wise K. L1 adaptive controller for air-breathing hypersonic vehicle with flexible body dynamics. In: Proceedings of the 2009 American Control Conference. Saint Louis, Missouri: IEEE, 2009. 3166-3171
[30]	Sigthorsson D O, Jankovsky P, Serrani A, Yurkovich S, Bolender M A, Doman D B. Robust linear output feedback control of an airbreathing hypersonic vehicle. Journal of Guidance, Control, and Dynamics, 2008, 31(4): 1052-1065
[31]	Ochi Y. Design of a flight controller for hypersonic flight experiment vehicle. Asian Journal of Control, 2004, 6(3): 353-361
[32]	Mooij E. Numerical investigation of model reference adaptive control for hypersonic aircraft. Journal of Guidance, Control, and Dynamics, 2001, 24(2): 315-323
[33]	Gibson T E, Crespo L G, Annaswamy A M. Adaptive control of hypersonic vehicles in the presence of modeling uncertainties. In: Proceedings of the 2009 American Control Conference. Saint Louis, Missouri: IEEE, 2009. 3178-3183
[34]	Gunnarsson K S, Jacobsen J O. Design and simulation of a parameter varying controller for a fighter aircraft. In: Proceedings of the 2001 AIAA Guidance, Navigation, and Control Conference and Exhibit. Montreal, Canada: American Institute of Aeronautics and Astronautics, 2001. AIAA 2001-4105
[35]	Wang Q, Stengel R F. Robust nonlinear control of a hypersonic aircraft. Journal of Guidance, Control, and Dynamics, 2000, 23(4): 577-585
[36]	Fiorentini L, Serrani A, Bolender M A, Doman D B. Nonlinear robust adaptive control of flexible air-breathing hypersonic vehicles. Journal of Guidance, Control and Dynamics, 2009, 32(2): 402-417
[37]	Serrani A, Zinnecker A M, Fiorentini L, Bolender M A, Doman D B. Integrated adaptive guidance and control of constrained nonlinear air-breathing hypersonic vehicle models. In: Proceedings of the 2009 American Control Conference. Saint Louis, Missouri: IEEE, 2009. 3172-3177
[38]	Xu H J, Mirmirani M, Ioannou P. Adaptive sliding mode control design for a hypersonic flight vehicle. Journal of Guidance, Control, and Dynamics, 2004, 27(5): 829-838
[39]	Rehman O U, Fidan B, Petersen I. Minimax LQR control design for a hypersonic flight vehicle. In: Proceedings of the 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Bremen, Germany: American Institute of Aeronautics and Astronautics, 2009. AIAA 2009-7291
[40]	Mu C X, Sun C Y, Yu X H. Observation and control for air-breathing hypersonic aircrafts based on sliding mode method. In: Proceedings of the 37th Annual Conference of the IEEE Industrial Electronics Society. Melbourne, Australia: IEEE, 2011. 3965-3970
[41]	Huang Y Q, Sun C Y, Qian C S, Wang L. Non-fragile switching tracking control for a flexible air-breathing hypersonic vehicle based on polytopic LPV model. Chinese Journal of Aeronautics, 2013, 26(4): 948-959
[42]	Huang Y Q, Sun C Y, Qian C S, Zhang J M, Wang L. Polytopic LPV modeling and gain-scheduled switching control for a flexible air-breathing hypersonic vehicle. Journal of Systems Engineering and Electronics, 2013, 24(1): 118-127
[43]	Sigthorsson D, Serrani A, Bolender M A, David D B. LPV control design for over-actuated hypersonic vehicles models. In: Proceedings of the 2009 AIAA Guidance, Navigation, and Control Conference and Exhibit. Lllinois, Chicago: American Institute of Aeronautics and Astronautics, 2009. AIAA 2009-6280
[44]	Gao Dao-Xiang, Sun Zeng-Qi, Luo Xiong, Du Tian-Rong. Fuzzy adaptive control for hypersonic vehicle via backstepping method. Control Theory and Applications, 2008, 25(5): 805-810 (高道祥, 孙增圻, 罗熊, 杜天容. 基于Backstepping的高超声速飞行器模糊自适应控制. 控制理论与应用, 2008, 25(5): 805-810)
[45]	Gao Dao-Xiang, Sun Zeng-Qi, Du Tian-Rong. Discrete-time controller design for hypersonic vehicle via back-stepping. Control and Decision, 2009, 24(3): 459-463, 467 (高道祥, 孙增圻, 杜天容. 高超声速飞行器基于Back-stepping的离散控制器设计. 控制与决策, 2009, 24(3): 459-463, 467)
[46]	Liu Yan-Bin, Lu Yu-Ping. Longitudinal inversion flight control based on backstepping for hypersonic vehicle. Control and Decision, 2007, 22(3): 313-317 (刘燕斌, 陆宇平. 基于反步法的高超音速飞机纵向逆飞行控制. 控制与决策, 2007, 22(3): 313-317)
[47]	Zong Q, Ji Y H, Zeng F L, Liu H L. Output feedback back-stepping control for a generic hypersonic vehicle via small-gain theorem. Aerospace Science and Technology, 2012, 23: 409-417
[48]	Zhou Z, Lin C F. Fuzzy logic based flight control system for hypersonic transporter. In: Proceedings of the 36th IEEE Conference on Decision and Control. San Diego, California: IEEE, 1997. 2730-2735
[49]	Xu H J, Mirmirani M, Ioannou P. Robust neural adaptive control of a hypersonic aircraft. In: Proceedings of the 2003 AIAA Guidance, Navigation, and Control Conference and Exhibit. Austin, Texas: American Institute of Aeronautics and Astronautics, 2003. AIAA 2003-5641
[50]	Meng B, Wu H X. Adaptive control based on characteristic model for a hypersonic flight vehicle. In: Proceedings of the 26th Chinese Control Conference. Zhangjiajie, Hunan: IEEE, 2007. 720-724
[51]	Adami T A, Zhu J, Bolender M A, Doman D B, Oppenheimer M. Flight control of hypersonic scramjet vehicles using a differential algebraic approach. In: Proceedings of the 2006 AIAA Guidance, Navigation, and Control Conference and Exhibit. Keystone, Colorado: American Institute of Aeronautics and Astronautics, 2006. AIAA 2006-6559
[52]	Adami T A, Zhu J. Control of a flexible, hypersonic scramjet vehicle using a differential algebraic approach. In: Proceedings of the 2008 AIAA Guidance, Navigation and Control Conference and Exhibit. Honolulu, Hawaii: American Institute of Aeronautics and Astronautics, 2008. AIAA 2008-7464
[53]	Mu Chao-Xu, Yu Xing-Huo, Sun Chang-Yin. Phase trajectory and transient analysis for nonsingular terminal sliding mode control systems. Acta Automatica Sinica, 2013, 39(6): 902-908 (穆朝絮, 余星火, 孙长银. 非奇异终端滑模控制系统相轨迹和暂态分析. 自动化学报, 2013, 39(6): 902-908)
[54]	Zhou Ying-Jiang, Wang Li, Sun Chang-Yin. Global asymptotic and finite-time stability for nonlinear systems. Acta Automatica Sinica, 2013, 39(5): 664-672 (周映江, 王莉, 孙长银. 一类非线性系统的全局渐近稳定和有限时间镇定. 自动化学报, 2013, 39(5): 664-672)
[55]	Zhang R M, Sun C Y, Zhang J M, Zhou Y J. Second-order terminal sliding mode control for hypersonic vehicle in cruising flight with sliding mode disturbance observer. Journal of Control Theory and Applications, 2013, 11(2): 299-305
[56]	Sun H B, Li S H, Sun C Y. Finite time integral sliding mode control of hypersonic vehicles. Nonlinear Dynamics, 2013, 73(1-2): 229-244
[57]	Sun H B, Li S H, Sun C Y. Robust adaptive integral-sliding-mode fault-tolerant control for airbreathing hypersonic vehicles. Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 2012, 226(10): 1344-1355
[58]	Li S H, Sun H B, Sun C Y. Composite controller design for an airbreathing hypersonic vehicle. Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 2012, 226(5): 651-664
[59]	Yang J, Li S H, Sun C Y, Guo L. Nonlinear-disturbance-observer-based robust flight control for airbreathing hypersonic vehicles. IEEE Transactions on Aerospace and Electronic Systems, 2013, 49(2): 1263-1275
[60]	Groves K P, Serrani A, Yurkovich S, Bolender M A, Doman D B. Anti-windup control for an air-breathing hypersonic vehicle model. In: Proceedings of the 2006 AIAA Guidance, Navigation, and Control Conference and Exhibit. Keystone, Colorado: American Institute of Aeronautics and Astronautics, 2006. AIAA 2006-6557
[61]	Vaddi S S, Sengupta P. Controller design for hypersonic vehicles accommodating nonlinear state and control constraints. In: Proceedings of the 2009 AIAA Guidance, Navigation, and Control Conference and Exhibit. Lllinois, Chicago: American Institute of Aeronautics and Astronautics, 2009. AIAA 2009-6286
[62]	Li Hui-Feng. Guidance and Control Technology of Hypersonic Aircrafts. Beijing: China Astronautic Publishing House, 2012 (李惠峰. 高超声速飞行器制导与控制技术. 北京: 中国宇航出版社, 2012)
[63]	Sun H B, Li S H, Sun C Y. Non-fragile adaptive fault-tolerant controller design for an airbreathing hypersonic vehicle. In: Proceedings of the 31st Chinese Control Conference. Hefei, China: IEEE, 2012. 453-458
[64]	Sun H B, Li S H, Sun C Y. Adaptive fault-tolerant controller design for airbreathing hypersonic vehicle with input saturation. Journal of Systems Engineering and Electronics, 2013, 24(3): 488-499
[65]	Fiorentini L, Serrani A, Bolender M A, Doman D B. Nonlinear robust/adaptive controller design for an air-breathing hypersonic vehicle model. In: Proceedings of the 2007 AIAA Guidance, Navigation and Control Conference and Exhibit. Hilton Head, South California: American Institute of Aeronautics and Astronautics, 2007. AIAA 2007-6329
[66]	Sun C Y, Huang Y Q, Qian C S, Wang L. On modeling and control of a flexible air-breathing hypersonic vehicle based on LPV method. Frontiers of Electrical and Electronic Engineering, 2012, 7(1): 56-68
[67]	Bolender M A, Doman D B. Flight path angle dynamics of air-breathing hypersonic vehicles. In: Proceedings of the 2006 AIAA Guidance, Navigation, and Control Conference and Exhibit. Keystone, Colorado: American Institute of Aeronautics and Astronautics, 2006. AIAA 2006-6692
[68]	Oppenheimer M W, Doman D B. Control of an unstable, nonminimum phase hypersonic vehicle model. In: Proceedings of the 2006 IEEE Aerospace Conference, Big Sky, Montana: IEEE, 2006. 1-7
[69]	Fiorentini L, Serrani A, Bolender M A, Doman D B. Nonlinear control of non-minimum phase hypersonic vehicle models. In: Proceedings of the 2009 American Control Conference. Saint Louis, Missouri: IEEE, 2009. 3160-3165
[70]	Yang Jun-Chun, Ni Mao-Lin. Design of guidance law for reentry vehicles based on the solution of Riccati equation. Aerospace Control, 2006, 24(4): 31-34 (杨俊春, 倪茂林. 基于Riccati方程解的再入飞行器制导律设计. 航天控制, 2006, 24(4): 31-34)
[71]	Carson J M III, Epstein M S, MacMynowski D G, Murray R M. Optimal nonlinear guidance with inner-loop feedback for hypersonic re-entry. In: Proceedings of the 2006 American Control Conference. Minneapolis, Minnesota: IEEE, 2006. 5782-5787
[72]	Zhang J, Xiao Y Z, Bi Z F. Guidance method based on multi-model prediction for re-entry vehicles. Acta Aeronautica Et Astronautica Sinica, 2008, 29(Suppl): S20-S25
[73]	Li Hui-Feng, Xie Ling. Reentry guidance law design for RLV based on predictor-corrector method. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(11): 1344-1348 (李惠峰, 谢陵. 基于预测校正方法的RLV再入制导律设计. 北京航空航天大学学报, 2009, 35(11): 1344-1348)
[74]	Lu P. Predictor-corrector entry guidance for low-lifting vehicles. Journal of Guidance, Control, and Dynamics, 2008, 31(4): 1067-1075
[75]	Xue S B, Lu P. Constrained predictor-corrector entry guidance. Journal of Guidance, Control, and Dynamics, 2010, 33(4): 1273-1281
[76]	Hu Jian-Xue, Chen Ke-Jun, Zhao Han-Yuan, Yu Meng-Lun. Hybrid entry guidance for reusable launch vehicles. Journal of Astronautics, 2007, 28(1): 213-217 (胡建学, 陈克俊, 赵汉元, 余梦伦. RLV再入混合制导方法研究. 宇航学报, 2007, 28(1): 213-217)
[77]	Wang Jun-Bo, Tian Yuan, Ren Zhang. Mixed guidance method for reentry vehicles based on optimization. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(6): 736-740 (王俊波, 田源, 任章. 基于最优化问题的混合再入制导方法. 北京航空航天大学学报, 2010, 36(6): 736-740)
[78]	Chen Gang, Kang Xing-Wu, Yan Gui-Rong, Chen Shi-Lu. Real time robust adaptive reentry guidance law based on pseudo-spectral method. Journal of System Simulation, 2008, 20(20): 5623-5626, 5634 (陈刚, 康兴无, 闫桂荣, 陈士橹. 基于伪谱方法的自适应鲁棒实时再入制导律研究. 系统仿真学报, 2008, 20(20): 5623-5626, 5634)
[79]	Tian B L, Zong Q. Optimal guidance for reentry vehicles based on indirect Legendre pseudospectral method. Acta Astronautica, 2011, 68(7-8): 1176-1184
[80]	Hu Jian-Xue, Chen Ke-Jun, Zhao Han-Yuan, Yu Meng-Lun. Comparisons between reference-trajectory and predictor-corrector entry guidances for RLVs. Journal of National University of Defense Technology, 2007, 29(1): 26-29, 34 (胡建学, 陈克俊, 赵汉元, 余梦伦. RLV再入标准轨道制导与轨道预测制导方法比较分析. 国防科技大学学报, 2007, 29(1): 26-29, 34)
[81]	Calhoun P C, Queen E M. Entry vehicle control system design for the mars science laboratory. Journal of Spacecraft and Rockets, 2006, 43(2): 324-329
[82]	Burken J J, Lu P, Wu Z L, Bahm C. Two reconfigurable flight-control design methods: robust servomechanism and control allocation. Journal of Guidance, Control, and Dynamics, 2001, 24(3): 482-493
[83]	He Cheng-Long, Chen Xin, Yang Yi-Dong. Mixed programming control allocation for reusable launch vehicles using dynamic inverse calculating. Systems Engineering and Electronics, 2010, 32(9): 1973-1976, 2008(贺成龙, 陈欣, 杨一栋. 一种动态逆解算的RLV混合规划控制分配研究. 系统工程与电子技术, 2010, 32(9): 1973-1976, 2008)
[84]	Hall C, Hodel A S, Hung J Y. Variable-structure PID control to prevent integrator windup. IEEE Transactions on Industrial Electronics, 2001, 48(2): 442-451
[85]	Johnson E N. Limited Authority Adaptive Flight Control. Atlanta: Georgia Institute of Technology, 2000
[86]	Lian B H, Hurtado J E. Adaptive backstepping control based autopilot design for reentry vehicle. In: Proceedings of the 2004 AIAA Guidance, Navigation, and Control Conference and Exhibit. Providence, Rhode Island: American Institute of Aeronautics and Astronautics, 2004. AIAA 2004-5328
[87]	Shtessel Y, Krupp D. Reusable launch vehicle trajectory control in sliding modes. In: Proceedings of the 1997 American Control Conference. Albuquerque, New Mexico: IEEE, 1997. 2557-2561
[88]	Shtessel Y, McDuffie J, Jackson M, Hall C, Gallaher M, Krupp D, et al. Sliding mode control of the X-33 vehicle in launch and re-entry modes. In: Proceedings of the 1998 AIAA Guidance, Navigation, and Control Conference and Exhibit. Boston, Massachusetts: American Institute of Aeronautics and Astronautics, 1998. AIAA 1998-4414
[89]	Shtessel Y, Hall C, Jackson M. Reusable launch vehicle control in multiple-time-scale sliding modes. Journal of Guidance, Control, and Dynamics, 2000, 23(6): 1013-1020
[90]	Shtessel Y, Hall C. Multiple time scale sliding mode control of reusable launch vehicles in ascent and descent modes. In: Proceedings of the 2001 American control conference. Arlington, Viraginia: IEEE, 2001. 4357-4362
[91]	Shtessel Y, Zhu J, Daniels D. Reusable launch vehicle attitude control using a time-varying sliding mode control technique. In: Proceedings of the 34th Southeastern Symposium on System Theory. Savannah, Georgia: IEEE, 2002. 81-85
[92]	Hall C, Shtessel Y. Sliding mode disturbance observer-based control for a reusable launch vehicle. In: Proceedings of the 2005 AIAA Guidance, Navigation, and Control Conference and Exhibit. San Francisco, California: American Institute of Aeronautics and Astronautics, 2005. AIAA 2005-6145
[93]	Hall C, Shtessel Y. Sliding mode disturbance observer-based control for a reusable launch vehicle. Journal of Guidance, Control, and Dynamics, 2006, 29(6): 1315-1328
[94]	Shtessel Y, Strott J, Zhu J. Time-varying sliding mode control with sliding mode observer for reusable launch vehicle. In: Proceedings of the 2003 AIAA Guidance, Navigation, and Control Conference and Exhibit. Austin, Texas: American Institute of Aeronautics and Astronautics, 2003. AIAA 2003-5362
[95]	Ning Guo-Dong, Zhang Shu-Guang, Fang Zhen-Ping. Entry control using sliding modes and state observer synthesis for reusable launch vehicle. Journal of Astronautics, 2007, 28(1): 69-76 (宁国栋, 张曙光, 方振平. 可重复使用航天器基于状态估计的再入飞行滑模控制器设计研究. 宇航学报, 2007, 28(1): 69-76)
[96]	Li Ke-Feng Tian Yuan, Ren Zhang. Advanced control method research for lift reentry flight. Aerospace Shanghai, 2006, 23(4): 27-29, 33 (黎科峰, 田源, 任章. 升力式再入飞行器的先进控制方法研究. 上海航天, 2006, 23(4): 27-29, 33)
[97]	Ji Peng-Fei, Zhou Jun. Variable structure attitude control algorithm of reentry vehicle. Computer Simulation, 2010, 27(4): 53-56 (及鹏飞, 周军. 再入飞行器变结构姿态控制律设计与仿真. 计算机仿真, 2010, 27(4): 53-56)
[98]	Zhu J, Banker B, Hall C. X-33 ascent flight control design by trajectory linearization---a singular perturbation approach. In: Proceedings of the 2000 AIAA Guidance, Navigation and Control Conference and Exhibit. Denver, Colorado: American Institute of Aeronautics and Astronautics, 2000. AIAA 2000-4159
[99]	Bevacqua T, Best E, Huizenga A, Cooper D, Zhu J. Improved trajectory linearization flight controller for reusable launch vehicles. In: Proceedings of the 42nd AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada: American Institute of Aeronautics and Astronautics, 2004. AIAA 2004-875
[100]	Zhang Chun-Yu, Jiang Chang-Sheng, Zhu Liang. Trajectory linearization control for an aerospace vehicle based on fuzzy disturbance observer. Journal of Astronautics, 2007, 28(1): 33-38 (张春雨, 姜长生, 朱亮. 基于模糊干扰观测器的空天飞行器轨迹线性化控制. 宇航学报, 2007, 28(1): 33-38)
[101]	Zhu L, Jiang C S, Zhang C Y. Adaptive trajectory linearization control for aerospace vehicle based on rbfnn disturbance observer. Acta Aeronautica Et Astronautica Sinica, 2008, 28(3): 673-677
[102]	Zhu Liang, Jiang Chang-Sheng, Xue Ya-Li. Robust adaptive trajectory linearization control for aerospace vehicle using single hidden layer neural networks. Acta Armamentarii, 2008, 29(1): 52-56 (朱亮, 姜长生, 薛雅莉. 基于单隐层神经网络的空天飞行器鲁棒自适应轨迹线性化控制. 兵工学报, 2008, 29(1): 52-56)
[103]	Zhu Liang. Robust Adaptive Control for Uncertain Nonlinear Systems and Its Applications to Aerospace Vehicles [Ph.D. dissertation], Nanjing University of Aeronautics and Astronautics, China, 2006 (朱亮. 空天飞行器不确定非线性鲁棒自适应控制 [博士学位论文], 南京航空航天大学, 中国, 2006)
[104]	Yan Dai-Wei, Gu Liang-Xian, Guan Qian-Shan, Sun Ping. Combat effectiveness modeling and evaluation of hypersonic cruise missiles. Acta Armamentarii, 2007, 28(6): 725-729 (阎代维, 谷良贤, 管千山, 孙平. 高超声速巡航导弹作战效能建模与评估. 兵工学报, 2007, 28(6): 725-729)
[105]	Gu Feng, He Yu-Qing, Han Jian-Da, Wang Yue-Chao. An active cooperative observation method for multi-robots in three dimensional environments. Acta Automatica Sinica, 2010, 36(10): 1443-1453 (谷丰, 何玉庆, 韩建达, 王越超. 三维环境中多机器人动态目标主动协作观测方法. 自动化学报, 2010, 36(10): 1443-1453)
[106]	Wang Lin, Wang Nan, Zhu Hua-Yong, Shen Lin-Cheng. Distributed fusion estimation algorithm for multi-UAVs cooperative sensing. Control and Decision, 2010, 25(6): 814-820 (王林, 王楠, 朱华勇, 沈林成. 一种面向多无人机协同感知的分布式融合估计方法. 控制与决策, 2010, 25(6): 814-820)
[107]	Xiao Song, Tan Xian-Si, Wang Hong, Li Zhi-Huai. Research on the detection system of near-space hypersonic vehicle. Winged Missiles Journal, 2012, (6): 28-31 (肖松, 谭贤四, 王红, 李志淮. 国外临近空间高超声速飞行器探测系统研究. 飞航导弹, 2012, (6): 28-31)
[108]	Li Chang-Xi, Bi Hong-Kui, Wang Hong, Zhang Bing. A target tracking algorithm for hypersonic aircraft in near space. Aerospace Electronic Warfare, 2012, (4): 10-13 (李昌玺, 毕红葵, 王红, 张兵. 一种临近空间高超声速目标跟踪算法. 航天电子对抗, 2012, (4): 10-13)
[109]	Wang Jian-Qing, Li Fan, Zhao Jian-Hui, Wan Cong-Mei. Summary of guidance law based on cooperative attack of multi-missile method. Flight Dynamics, 2011, 29(4): 6-10 (王建青, 李帆, 赵建辉, 万聪梅. 多导弹协同制导律综述. 飞行力学, 2011, 29(4): 6-10)
[110]	Zhao S Y, Zhou R. Multi-missile cooperative guidance using coordination variables. Acta Aeronautica et Astronautica Sinica, 2008, 29(6): 1605-1611
[111]	Peng Chen, Liu Xing, Wu Sen-Tang, Li Meng. Consensus problems in distributed cooperative terminal guidance time of multi-missiles. Control and Decision, 2010, 25(10): 1557-1561, 1566 (彭琛, 刘星, 吴森堂, 李甍. 多弹分布式协同末制导时间一致性研究. 控制与决策. 2010, 25(10): 1557-1561, 1566)
[112]	Harl N, Balakrishnan S N. Impact time and angle guidance with sliding mode control. IEEE Transactions on Control Systems Technology, 2012, 20(6): 1436-1449
[113]	Fan Z E, Shi X J, Pan C P, Gu W J. A finite-time convergent variable structure guidance law with impact angle constraint. Intelligence Computation and Evolutionary Computation, Advances in Intelligent Systems and Computing. Berlin Heidelberg: Springer-Verlag, 2013, 180: 513-519
[114]	Oh S, Schenato L, Chen P, Sastry S. Tracking and coordination of multiple agents using sensor networks: system design, algorithms and experiments. Proceedings of the IEEE, 2007, 95(1): 234-254
[115]	Olfati-Saber R, Jalalkamali P. Collaborative target tracking using distributed Kalman filtering on mobile sensor networks. In: Proceedings of the 2011 American Control Conference. San Francisco, California: IEEE, 2011. 1100-1105
[116]	Wang X L, Hong Y G, Jiang Z P. Coverage tracking of a moving target by a group of mobile agents. In: Proceedings of the 7th Asian Control Conference. Hong Kong, China: IEEE, 2009. 332-337