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第3期 马正华,等:四旋翼飞行器自适应反演姿态控制 459. 12]PALUNKO P,FIERRO F.Adaptive control of a quadrotor 参考文献: with dynamic changes in the center of gravity[C]//Pro- [1]MUNGUIA R,GRAU A.An attitude and heading reference ceedings of the 18th IFAC World Congress.Milano,Italy, system AHRS)based in a dual filter [C]//2011 IEEE 2011:2626-2631. Conference on Emerging Technologies Factory Automation [13]ALTUG E,OSTROWSKI J P,TAYLOR C J.Quadrotor ETFA).Toulouse,French.2011:1-8. control using dual camera visual feedback C ]//2003 [2]LEISHMAN J G.The breguet-richet quad-rotor helicopter of IEEE International Conference on Robotics Automation. 1907[J].AHS International Directory,2001:1-4. Taipei,China:4294-4299. [3]BOUABDALLAH S,SIEGWART R.Full Control of a [14]JONES D I,WHITWORTHB CC,EARPC G K,et al.A quadrotor[C]//Proceedings of the IEEE/RSJ International laboratory test-bed for an automated power line inspection Conference on Intelligent Robots and Systems.San Diego, system[J].Control Engineering Practice,2005,13(7): USA:EEE,2007:153-158. 835-851. [4]GONZALEZ-VAZQUEZ S,MORENO-VALENZUELA J.A [15]HAMEL T,MAHONY R,LOZANO R,et al.Dynamic new nonlinear Pl/PID controller for quadrotor posture regu- modeling and configuration stabilization for an X4-Flyer lationC//2010 Electronics,Robotics and Automotive [C]//Proceeding of IFAC 15th Triennial World Congress. Mechanics Conference.Morelos,Mexico,2010:642-647. Barcelona,Spain,2002:665-670. [5]乔维维.四旋冀飞行器飞行控制系统研究与仿真[D]. [16]ZHANG Y M,CHAMSEDDINE A,RABBATH C A,et al. 太原:中北大学,2012:157-168. Development of advanced FDD and FTC,techniques with QIAO Weiwei.Research and simulation on four rotor heli- application to an unmanned quadrotor helicopter testbed copter flight control system[D].Taiyuan,China:North U. [J].Journal of the Franklin Institute,2013,350(9): niversity of China,2012:157-168. 2396-2422. [6]岳基隆.四旋翼无人机自适应控制方法研究[D].长沙: 作者简介: 国防科学技术大学,2010:128-135. 马正华,男,1962年生,教授,主要 YUE Jilong.Research on adaptive control method for 研究方向为嵌入式系统应用、计算机控 quadrotor UAV[D].Changsha,China:National University 制技术、电力电子技术,曾获江苏省科 of Defense Technology,2007:128-135. 技进步三等奖2项,中国机械工业联合 [7]SALIH A L,MOGHAVVEMI M,MOHAMED H A F,et al. 会科技进步三等奖1项。发表学术论 Flight PID controller design for a UAV quadrotor[]Scien- 文100余篇。 tific Research and Essays,2010,5(23):3660-3667. [8]毕胜.变结构飞行器的多刚体建模和姿态控制[D].合 张倩倩,女,1988年生,硕士研究 肥:中国科学技术大学,2011:5-20. 生,主要研究方向为计算机软件与理 BI Sheng.Multi-rigid-body modeling and attitude control of 论、无人机控制系统。 variable structure aircraft[D].Hefei,China:University of Science and Technology of China,2011:5-20. [9]LEE H.Robust adaptive fuzzy control by backstepping for a class of MIMO nonlinear systems[]].IEEE Transactions on Fuzzy Systems,2011,19(2):265-275. 陈岚萍,女,1974年生,副教授,博 [10]YOON S H,KIM Y D,PARK S H.Constrained adaptive 士,主要研究方向为复杂系统稳定性与 backstepping controller design for aircraft landing in wind 跟踪控制、生产过程的优化控制及运动 disturbance and actuator stuckJ.International Journal of 轨迹跟踪控制。完成或参与国家、省级 Aeronautical and Space Sciences,2012,13(1):74-89. 课题项目4项,主持或参与其他各级各 [11]BOUSSERHANE I K,Hazzab A,MAZARI B,et al.Mov- 类课题5项。发表学术论文20余篇. er position control of linear induction motor drive using a- 被SCI检索3篇、EI检索10篇。 daptive backstepping controller with integral action [J]. Tamkang Journal of Science and Engineering,2010,12 (1):17-18.参考文献: [1]MUNGUIA R, GRAU A. An attitude and heading reference system ( AHRS) based in a dual filter [ C] / / 2011 IEEE Conference on Emerging Technologies & Factory Automation (ETFA). Toulouse, French, 2011: 1⁃8. [2]LEISHMAN J G. The breguet⁃richet quad⁃rotor helicopter of 1907[J]. AHS International Directory, 2001: 1⁃4. [3 ] BOUABDALLAH S, SIEGWART R. Full Control of a quadrotor[C] / / Proceedings of the IEEE/ RSJ International Conference on Intelligent Robots and Systems. San Diego, USA: IEEE, 2007: 153⁃158. [4] GONZÁLEZ⁃VÁZQUEZ S, MORENO⁃VALENZUELA J. A new nonlinear PI/ PID controller for quadrotor posture regu⁃ lation [ C] / / 2010 Electronics, Robotics and Automotive Mechanics Conference. Morelos, Mexico, 2010: 642⁃647. [5]乔维维. 四旋翼飞行器飞行控制系统研究与仿真[D]. 太原: 中北大学, 2012: 157⁃168. QIAO Weiwei. Research and simulation on four rotor heli⁃ copter flight control system[D]. Taiyuan, China: North U⁃ niversity of China, 2012: 157⁃168. [6]岳基隆. 四旋翼无人机自适应控制方法研究[D]. 长沙: 国防科学技术大学, 2010: 128⁃135. YUE Jilong. Research on adaptive control method for quadrotor UAV[D]. Changsha, China: National University of Defense Technology, 2007: 128⁃135. [7]SALIH A L, MOGHAVVEMI M, MOHAMED H A F, et al. Flight PID controller design for a UAV quadrotor[J]. Scien⁃ tific Research and Essays, 2010, 5(23): 3660⁃3667. [8]毕胜. 变结构飞行器的多刚体建模和姿态控制[D]. 合 肥: 中国科学技术大学, 2011: 5⁃20. BI Sheng. Multi⁃rigid⁃body modeling and attitude control of variable structure aircraft[D]. Hefei, China: University of Science and Technology of China, 2011: 5⁃20. [9]LEE H. Robust adaptive fuzzy control by backstepping for a class of MIMO nonlinear systems[J]. IEEE Transactions on Fuzzy Systems, 2011, 19(2): 265⁃275. [10]YOON S H, KIM Y D, PARK S H. Constrained adaptive backstepping controller design for aircraft landing in wind disturbance and actuator stuck[J]. International Journal of Aeronautical and Space Sciences, 2012, 13(1): 74⁃89. [11]BOUSSERHANE I K, Hazzab A, MAZARI B, et al. Mov⁃ er position control of linear induction motor drive using a⁃ daptive backstepping controller with integral action [ J ]. Tamkang Journal of Science and Engineering, 2010, 12 (1): 17⁃18. [12]PALUNKO P, FIERRO F. Adaptive control of a quadrotor with dynamic changes in the center of gravity [ C] / / Pro⁃ ceedings of the 18th IFAC World Congress. Milano, Italy, 2011: 2626⁃2631. [13] ALTUG E, OSTROWSKI J P, TAYLOR C J. Quadrotor control using dual camera visual feedback [ C ] / / 2003 IEEE International Conference on Robotics & Automation. Taipei, China: 4294⁃4299. [14]JONES D I, WHITWORTHB C C, EARPC G K, et al. A laboratory test-bed for an automated power line inspection system[J]. Control Engineering Practice, 2005, 13( 7): 835⁃851. [15] HAMEL T, MAHONY R, LOZANO R, et al. Dynamic modeling and configuration stabilization for an X4⁃Flyer [C] / / Proceeding of IFAC 15th Triennial World Congress. Barcelona, Spain, 2002: 665⁃670. [16]ZHANG Y M, CHAMSEDDINE A, RABBATH C A, et al. Development of advanced FDD and FTC, techniques with application to an unmanned quadrotor helicopter testbed [J]. Journal of the Franklin Institute, 2013, 350 ( 9): 2396⁃2422. 作者简介: 马正华,男,1962 年生,教授,主要 研究方向为嵌入式系统应用、计算机控 制技术、电力电子技术,曾获江苏省科 技进步三等奖 2 项,中国机械工业联合 会科技进步三等奖 1 项。 发表学术论 文 100 余篇。 张倩倩,女,1988 年生,硕士研究 生,主要研究方向为计算机软件与理 论、无人机控制系统。 陈岚萍,女,1974 年生,副教授,博 士,主要研究方向为复杂系统稳定性与 跟踪控制、生产过程的优化控制及运动 轨迹跟踪控制。 完成或参与国家、省级 课题项目 4 项,主持或参与其他各级各 类课题 5 项。 发表学术论文 20 余篇, 被 SCI 检索 3 篇、EI 检索 10 篇。 第 3 期 马正华,等:四旋翼飞行器自适应反演姿态控制 ·459·
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