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	Control Platform Design and Experiment of A Quadrotor 会议论文 OAI收割 2013 32nd Chinese Control Conference, Xi'an, China, July 26-28, 2013 作者: Jiang J(姜军); Qi JT(齐俊桐); Song DL(宋大雷) 收藏 \| 浏览/下载：29/0 \| 提交时间：2013/12/26 Quadrotor control platform design flight experiments
	微小型直升机姿态估计和鲁棒控制技术研究学位论文 OAI收割工学博士, 中国科学院自动化研究所: 中国科学院研究生院, 2012 作者: 常冠清收藏 \| 浏览/下载：60/0 \| 提交时间：2015/09/02 微小型直升机姿态估计 EKF SR-UKF 自抗扰控制 Backstepping 自适应模糊系统飞控系统平台 Miniature Helicopters Attitude Estimation EKF SR-UKF ADRC Backstepping Adaptive Fuzy System Flight Control platform
	Dynamic coupling analysis and modeling for stabilized platform of rolling-pitching seeker (EI CONFERENCE) 会议论文 OAI收割 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China 作者: Liu H.; Liu H.; Liu H. 收藏 \| 浏览/下载：13/0 \| 提交时间：2013/03/25 Missile's attitude change will be delivered to visual axis through stabilized platform during maneuvering flight and the missile vibration will be an interference source to visual axis stabilization. In order to solve this problem the coupling relationship between missile attitude and visual axis is obtained by Coordinate transformation. When the seeker stably tracks a target the angular velocity of visual axis in inertial space is zero so the relative angular velocity of roll axis and pitch axis can be derived for servo control. According to Oura dynamics equation the dynamic models of roll axis and pitch axis were established and kinetic equations of two axises were obtained. The dynamic models can provide theoretical basis to developing research of servo control system and structural optimization design of stabilized platform. Finally some measures could reduce the dynamic coupling between the framework was given. 2011 IEEE.