期刊文献+

事件触发机制下室内飞行器的姿态跟踪控制

Attitude Tracking Control of Indoor Aircraft under Event Triggered Mechanism
下载PDF
导出
摘要 室内环境下,针对惯性定位中传感器通过周期采样控制器采样频率高,造成采样信号的冗余,控制器节点对这些采样信号进行不必要计算,导致计算资源浪费的问题,现提出视觉惯性融合定位下的事件触发机制,构造事件触发控制器。首先建立室内四旋翼的动力学模型,在ROS中模拟视觉惯性融合定位算法,通过实验平台验证。其次以滚转角系统为例,用反步法设计控制器,并用Lyapunov稳定性理论证明系统稳定性。实验结果显示:在室内特征不明显情况下,飞行器在实际飞行过程中有较好的准确性,且3s内周期采样控制器采样3000次,所设计的事件触发仅需触发150次就可得到相同的跟踪效果,即此设计的事件触发控制器减少了飞行器内部的计算量,极大的节约了通讯资源。 In indoor environment,the sampling frequency of sensors passing through the periodic sampling control-ler in inertial positioning is high,which leads to the redundancy of sampling signals,and the unnecessary calculation of these sampling signals by the controller nodes leads to the waste of computing resources.In this paper,an event triggering mechanism based on visual inertial fusion positioning is proposed,and an event triggering controller is con-structed.Firstly,the dynamic model of indoor quadrotor was established,and the visual inertial fusion positioning algo-rithm was simulated in ROS,which was verified by the experimental platform.Secondly,taking the roll angle system as an example,the controller was designed by backstepping method,and the stability of the system was proved by Lya-punov stability theory.The experimental results show that the aircraft has good accuracy in the actual flight process when the indoor characteristics are not obvious,and the periodic sampling controller samples 3,000 times in 3s.The designed event trigger only needs to trigger 150 times to get the same tracking effect,that is,the designed event trigger controller reduces the internal calculation of the aircraft and greatly saves the communication resources.
作者 邓志良 袁玉雯 DENG Zhi-liang;YUAN Yu-wen(School of Automation,Nanjing University of Information Science&Technology,Nanjing Jiangsu 210044,China)
出处 《计算机仿真》 北大核心 2023年第11期22-26,81,共6页 Computer Simulation
基金 国家自然科学基金(51875293) 电子信息控制重点实验室开放基金项目(6142105190308)。
关键词 姿态跟踪控制 视觉惯性融合 事件触发机制 事件触发控制 Attitude tracking control Visual inertial fusion Event triggering mechanism Event triggered control
  • 相关文献

参考文献10

二级参考文献56

  • 1杜小菁,陈洪,王欣,李怀建.基于SINS解算的行人导航技术发展综述[J].战术导弹技术,2020(1):113-120. 被引量:5
  • 2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[J].宇航学报,2007,28(1):33-38. 被引量:12
  • 3KIM Jinhyun, KANG Minsung, PARK Sangdeok. Accurate modeling and robust hovering control for a Quadrotor VTOL aircraft [ J ]. Journal of Intelligent and Robotic Systems, 2010, 57: 9-26.
  • 4LARAA D, ROMEROA G, SANCHEZ A, et al. Robustness margin for attitude control of a four rotor mini-rotorcraft: case of study[J]. Mechatronics, 2010, 20(1): 143-152.
  • 5ALEXIS K, NIKOLAKOPOULOS G, TZES A. Switching model predictive attitude control for a Quadrotor helicopter subject to atmospheric disturbances [ J ]. Control Engineer- ing Practice, 2011, 19(10) : 1195-1027.
  • 6ZEMALACHE K M, MAAREF H. Controlling a drone: Com- parison between a based model method and a fuzzy inference system[J]. Applied Soft Computing, 2009, 9(2) : 553-562.
  • 7ERESEN A, IMAMOGLU N, ONDEREFE M. Autonomous Quadrotor flight with vision-based obstacle avoidance in vir- tual environment [ J ]. Expert Systems with Applications, 2012, 39( 1 ) : 894-905.
  • 8RAFFO G V, ORTEGA M G, RUBIO F R. An integral predictive/nonlinear control structure for a Quadrotor heli- copter[J]. Automatica, 2010, 46(1) : 29-39.
  • 9MICHAEL N, MELLINGER D, LINDSEY Q, et al. The GRASP multiple micro UAV testbed [ J ]. IEEE Robotics & Automation Magazine, 2010, 17 (3) : 56-.65.
  • 10XU Rong, OZGUNER U. Sliding mode control of a class of underactuated systems [ J ]. Automatica, 2008, 44 ( 1 ) : 233-241.

共引文献103

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部