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- Application of VSC to Missile Attitude Control Servo System 导弹姿态控制伺服系统的变结构控制
- Application of a New Control Law to Missile Attitude Control System 新型变结构控制律在导弹姿态控制系统中的应用
- Study on Dynamic Measurement of Missile Attitude Control System 导弹姿态控制系统动态测试研究
- ROBUST STABILITY ANALYSIS ON MISSILE ATTITUDE CONTROL SYSTEM 导弹姿态控制系统鲁棒稳定性分析
- Discrete VS Control of Digital Missile Attitude Control System 数字式姿态控制系统的离散变结构控制
- Determination of the Optimal Testing Points for Missile Attitude Control System 导弹姿态控制系统最佳测试点的选取
- Study on Global Variable Structure Adjuster of Missile Attitude Control System 导弹姿态全程滑态变结构模型跟踪控制系统设计
- Discrete Variable Structure Control of Missile Attitude Control System 数字式导弹姿态控制系统的变结构控制
- Application of Optimal Control Using Direct Side Force in Missile Attitude Control System 最优控制与姿控喷流在导弹姿态控制中的应用
- The Variable Structure Adaptive Control and its Application to Missile Attitude Control System 战略导弹姿态系统的变结构自适应控制研究
- Missile attitude control system 导弹姿态控制系统
- Missile attitude control 导弹姿态控制
- The attitude control system of maneuver missile head is designed by applyi ng nonlinear decoupling control law. 然后采用非线性解耦控制理论设计了机动弹头的姿态控制系统。
- In order to effectively adjust attitude motion of interceptor missile by combine control, an attitude control method was presented. 摘要为了有效地调整复合控制拦截弹的姿态运动,提出了一个姿态控制方法。
- Abstract In order to effectively adjust attitude motion of interceptor missile by combine control, an attitude control method was presented. 摘要 为了有效地调整复合控制拦截弹的姿态运动,提出了一个姿态控制方法。
- A novel method of fuzzy proportional-integral-differential (PID) control by GA is designed for the attitude control system of three-axis-stable mass moment missile in this paper. 摘要针对三轴稳定的质量矩导弹姿态控制系统,提出了一种基于遗传算法进行参数寻优的模糊PID控制方法。
- Large angle attitude control law is investigated in this paper for agile turn of an advanced air-to-air missile that has high off-boresight or over the shoulder capability. 为研究具有大离轴角及越肩发射能力的先进空空导弹敏捷转弯方法,研究了空空导弹的大角度姿态机动控制律。
- Attitude control is obtained by gimballing the engine up to ±7 degrees. 姿态控制是由发动机摆动而得到的,摆动度最大为±7°。
- Third, multi-duty direction pattern microminiaturized attitude control module. 三是多任务指向模式的微型化姿控模块。
- For strapdown imaging homing seeker system,the mapping relation from body line-of-sight(LOS) angles and missile attitude angles to inertial LOS angles is described. Then its Jacobin matrix and error transfer equations are derived. 针对捷联成像寻的器,首先给出体视线和弹体姿态到惯性视线的映射关系,然后通过推导映射函数的雅克比矩阵,给出了从体视线和弹体姿态到惯性视线的误差传递公式。
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