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- Abstract: Based on the theory of feedback-linearization and the simplified bank-to-turn (BTT) control design model, a BTT missile autopilot design method is presented. 文摘:提出基于反馈线性化理论的BTT导弹自动驾驶仪设计方法。
- Based on the theory of feedback-linearization and the simplified bank-to-turn (BTT) control design model, a BTT missile autopilot design method is presented. 提出基于反馈线性化理论的BTT导弹自动驾驶仪设计方法。
- R. T. Reichert, "Advance missile autopilot design," Theory and Application of Robust Multivariable Control Short Course, The John Hopkins University Applied Physics Laboratory , September 11-14, 1989. 彭昭伟，钢板滚压控制系统分析及设计，私立元智工学院电资所硕士论文1997.
- The method of missile autopilot design is proposed in this paper.Using some missile data the autopilot based on mixed sensitivity is designed.The simulation is done to the missile system. 研究了导弹制导回路鲁棒自动驾驶仪设计的理论与方法,并结合某型导弹进行了混合灵敏度自动驾驶仪的设计及仿真。
- BTT Missile Autopilot Design Using Integral LQG/LTR Control BTT导弹自动驾驶仪LQG/LTR积分控制设计
- BTT missile autopilot design based on dynamic inversion 基于动态逆的BTT导弹自动驾驶仪设计
- The method is applied to the design of a bank-to-turn (BTT) missile autopilot. 最后，将该方法应用于某BTT导弹自动驾驶仪的设计。
- Missile autopilot design 导弹自动驾驶仪设计
- Satisfactory results in the design of the BTT missile autopilot are obtained by using this method. 使用这种方法设计BTT导弹自动驾驶仪获得了满意的结果。
- A tracking control technique is applied to autopilot design of a tail-controlled STT missile system with coupling among channels. 基于变结构自适应控制理论，提出一种新的STT导弹自动驾驶仪三通道独立设计方法。
- According to the work and test principle of some air defense missile autopilot, an autopilot test facility is developed. 摘要根据某型防空导弹自动驾驶仪的工作原理和测试原理，研制了该驾驶仪测试设备；
- According to the work principle of some missile autopilot, the automatic test system of the missile autopilot based on the virtual instrument is developed. 摘要根据某型导弹自动驾驶仪的工作原理和测试原理，研制了基于虚拟仪器的导弹驾驶仪测试系统；
- Adaptive Autopilot Design for Air Defense Missile 某型防空导弹自适应自动驾驶仪设计
- In order to avoid cross couplings between the vertical and lateral motion,decoupling control of a double-channel control rolling missile autopilot was studied. 为消除旋转导弹自旋所带来的纵向与侧向运动的交叉耦合,进行了双通道控制旋转导弹自动驾驶仪回路解耦控制研究。
- CAD PACKAGE FOR AUTOPILOT DESIGN OF BTT MISSILE BTT导弹自动驾驶仪设计的CAD程序包
- Grimble M. J., Zhang Y. and Katebi M. R., -Based Ship Autopilot Design, Proceedings, 10th Symposium on Ship Control Systems, Ottawa, Canada, pp.2.51-2.66, 1993. 张仕东，线性时变系统控制器之设计及船舶上之应用，国立成功大学造船工程研究所硕士论文，1993。
- Based on the time-varying sliding-mode variable structure adaptive control theories, a new coordinate coupling autopilot design scheme for BTT missiles is proposed. Design for roll channel and pitch/yaw coupling channel is also analised respectivly. 针对倾斜转弯导弹的具体特点, 提出了一种基于模型参考时变全程滑态变结构控制理论的协调式耦合自动驾驶仪的设计方法, 并分别针对滚转通道、俯仰/偏航耦合通道进行了设计分析;
- Dual Sliding Mode Variable Structure Control Design for BTT Missile Autopilot 双滑模变结构控制的BTT导弹自动驾驶仪设计研究
- Model Reference Variable Structure Autopilot Design for Homing Missile 一种寻的制导导弹模型参考变结构自动驾驶仪的设计
- Autopilot design of roll channel for BTT missiles BTT导弹滚动通道自动驾驶仪设计
