期刊文献+

基于CAN网络小型直升机自动驾驶仪硬件及导航系统设计 被引量:2

Design hardware and navigation system for an autopilot of small helicopter based on CAN net
下载PDF
导出
摘要 本文介绍一种基于CAN网络的无人直升机自动驾驶仪的硬件系统结构与姿态导航原理。此系统采用GPS+INS组合导航系统,通过非线性卡尔曼滤波[1]计算飞机姿态与导航信息。
作者 赵涛 汪滔
机构地区 哈尔滨工业大学
出处 《制造业自动化》 北大核心 2010年第2期81-83,101,共4页 Manufacturing Automation
  • 相关文献

参考文献2

  • 1R.E.Kalman.A New Approach to Linear Filtering and Prediction Problems. Transactions of the ASME-Journal of Basic Engineering. 1960,82(Series D):35-45.
  • 2S. Julier,J.Uhlmann,H.Durrant.A New Approach for Filtering Nonlinear Systems.Proceedings of American Control Conference.1995:1628-1632.

同被引文献16

  • 1段镖,严峰,赖水清.基于FlightGear的无人直升机飞行控制系统仿真环境建设[J].直升机技术,2010(4):58-63. 被引量:6
  • 2Yi-Rui Tang, Yangmin Li. Development of a laboratory HILS testbed system for small UAV helicopters [C]// Proceedings of the 6th IASTED International Conference on Biomechanics; Proceedings of the Second IASTED International Conference on Robotics. Pittsburgh, USA: ACTA Press, 2011: 428-436.
  • 3Seongpil Kim, Agus Budiyono. Control system design and testing for a small-scale autonomous helicopter [J].Aircraft Engineering and Aerospace Technology (S0002-2667), 2010, 82(6): 353-359.
  • 4Bryan Godbolt. Experimental Validation of a Helicopter Autopilot Design using Model-Based PID Control [J]. Journal of Intelligent & Robotic Systems (S0921-0296), 2013, 70(1/4): 385-399.
  • 5Johannes Hofmann, Antje Dittmer. Model-based control of the flying helicopter simulator: evaluating and optimizing the feedback controller [J]. CEAS Aeronautical Journal (S 1869-5582), 2011, 2(1/4): 43-56.
  • 6Advanced Rotorcraft Technology, Inc. FLIGHTLAB Theory Manual, Volume I [M]. Charleston, USA: Advanced Rotorcraft Technology, Inc. 2011: 7-180.
  • 7He Chengjian. Finite State Dynamic Wake Interference Modeling for Rotorcraft Simulation [C]// American Helicopter Society 53rd Annual Forum, Virginia Beach, Virginia, USA: AHS, 1997: 973-987.
  • 8GJB5449-2005.直升机飞行模拟器通用要求[S].
  • 9严峰,赖水清,李林华.小型无人直升机发动机控制设计[J].系统仿真学报,2009,21(3):830-831. 被引量:4
  • 10袁东,杨生民,孙传伟.直升机飞行模拟器及其特点[J].系统仿真学报,2009,21(9):2571-2573. 被引量:8

引证文献2

二级引证文献2

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