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Variable stability system control law development for in-flight simulation of pitch/roll/yaw rate and normal load

机译：可变稳定性系统控制规律开发，用于俯仰/滚动/横摆率的飞行模拟和正常载荷

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Joon Soo Ko; Sungsu Park;
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年度 2014
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1. Analysis of Roll-Yaw Control Law Applied to the Initial Attitude Acquisition of Spacecraft with Single Pitch Wheel [J] . Yiing-Yuh Lin, Chin-Tzuo Wang Journal of the Chinese Society of Mechanical Engineers. Series C . 2005,第3期

机译：横摆控制律在单桨轮航天器初始姿态获取中的应用
2. Analysis of Roll-Yaw Control Law Applied to the Initial Attitude Acquisition of Spacecraft with Single Pitch Wheel [J] . Yiing-Yuh Lin, Chin-Tzuo Wang Journal of the Chinese Society of Mechanical Engineers, Series C: Transactions of the Chinese Society of Mechanical Engineers . 2005,第3期

机译：单桨轮航天器初始姿态获取中的横摆控制律分析
3. Development of a simple system for the simultaneous measurement of pitch, yaw and roll angular errors of a linear stage [J] . Chien-Hung Liu, Wen-Yuh Jywe, Chao-Kwai Chen The International Journal of Advanced Manufacturing Technology . 2005,第7a8期

机译：开发用于同时测量线性平台的俯仰，偏航和侧倾角误差的简单系统
4. Development of Integrated Control of Electronic Stability Control, Continuous Damping Control and Active Anti-Roll Bar for Vehicle Yaw Stability [C] . Hyundong Her, Kyongsu Yi, Jeeyoon Suh, IFAC Symposium on Advances in Automotive Control . 2013

机译：开发电子稳定控制的集成控制，用于车辆偏航稳定性的连续阻尼控制和活性防辊杆
5. Roll, Pitch and Yaw Torque Control for a Robotic Bee [D] . Finio, Benjamin Michael. 2012

机译：用于机器人蜜蜂的卷筒，俯仰和偏航扭矩控制
6. Integrated Chassis Control of Active Front Steering and Yaw Stability Control Based on Improved Inverse Nyquist Array Method [O] . Bing Zhu, Yizhou Chen, Jian Zhao -1

机译：基于改进逆奈奎斯特阵列方法的主动前转向和底盘稳定控制的集成底盘控制
7. Development of a Variable Stability Flight Simulation Facility Re-engineering of Flight Control Loading and Motion Systems [O] . Scamps Alexander 2003

机译：飞行控制加载和运动系统的可变稳定性飞行仿真设施的重新设计
8. Evaluation and Wind Tunnel Tests of the 4,000-lb (Normal-Force) Pitch/Yaw and Roll-Damping Stability Balance Systems for Measuring Direct, Cross, and Cross-Coupling Derivatives [R] . Buchanan, T. D., Coulter, S. M., Marquart, E. J. 1981

机译：用于测量直接，交叉和交叉耦合衍生物的4,000磅（法向力）俯仰/偏转和阻尼稳定平衡系统的评估和风洞测试

Variable stability system control law development for in-flight simulation of pitch/roll/yaw rate and normal load

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