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- This dissertation studies the applications of backstepping control design method on spacecraft attitude control system. 本论文研究退步控制设计方法在航天器姿态控制系统中的应用问题。
- The spacecraft attitude control system is designed via a backstepping method,considering the attitude dynamic model on conditions that flywheels are adapted as actuatoss. 研究了航天器的姿态控制问题。考虑了飞轮作为执行机构的姿态动力学模型,应用退步控制理论设计了姿态控制算法。
- The steering laws of single gimbal control moment gyms (SGCMGs) are analyzed and compared for a spacecraft attitude control system based on the singular value decomposition (SVD) theory. 摘要基于奇异值分解理论,对航天器姿态控制系统中使用的单框架控制力矩陀螺(SGCMG)的操纵律进行了分析和比较研究。
- Adaptive neural-network-based inverse method and its application in spacecraft attitude control 航天器姿态的神经网络动态逆控制
- Spacecraft attitude control using parallel-gimbaled variable speed control moment gyros group 采用平行构型变速控制力矩陀螺群的航天器姿态控制
- Three-axis Air-bearing Table and Hardware-in-the-loop Simulation of Spacecraft Attitude Control System 三轴气浮转台与空间飞行器姿控半实物仿真
- spacecraft attitude control 航天器姿态控制
- A Fuzzy Neural Network Controller and Its Application Study for the Spacecraft Attitude Control System 模糊神经网络控制器及其在航天器姿态控制系统中的应用研究
- Nonlinear Robust Decentralized Controller Design for Spacecraft Attitude Control System 航天器姿态的非线性鲁棒分散控制器设计
- Here, we integrate both of them and propose reliable VSC control schemes to spacecraft attitude tracking problems. 另一方面,随著航空及工业界对可靠度的要求增加,有关可靠度控制的研究在这几年也成为一个非常热门的议题。
- The Attitude Control System( ACS) software is responsible for maintaining the attitude of the spacecraft. 姿态控制系统(CS)件负责维护航空器的姿态。
- Reaction fly-wheel is the implementary element of the poser control system of the space vehicle.The control system of servo motor plays an important role in spacecraft attitude. 摘要反作用飞轮是航天空间飞行器姿态控制系统的执行机构,其驱动电动机伺服系统性能优劣对飞行器的姿态有至关重要的作用。
- The paper mainly evaluates the technique of attitude control by simulating and fuzzy reasoning methods so as to research its infection to operation efficiency of spacecraft. 主要通过仿真方法和模糊推理方法对关键技术之一的姿态控制技术进行评估分析,研究其对航天器轨道机动效能的影响。
- In terms of this characteristic, the three-dimensional attitude control problem of the rigid spacecraft with three manipulators is discussed in the paper. 利用这一特性讨论了带空间机械臂的刚体航天器三维姿态运动的控制问题。
- ABSTRACT:Reaction fly-wheel is the implementary element of the poser control system of the space vehicle.The control system of servo motor plays an important role in spacecraft attitude. 摘要:反作用飞轮是航天空间飞行器姿态控制系统的执行机构,其驱动电动机伺服系统性能优劣对飞行器的姿态有至关重要的作用。
- Abstract: In this paper,a sliding mode control(SMC) method is derived and applied to a spacecraft attitude tracking system in the presence of parameter variations and external disturbances. 文摘:对于参数不确定和外部扰动的空间飞行器姿态跟踪系统,本文提出了采用滑模控制的方法。
- 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°。
- Topics extend to analysis of both aircraft flight dynamics and spacecraft attitude dynamics, based upon presented principles and equations of motion. 课题扩展分析了航天器飞行动力学和太空船飞行姿态动力学,这些建立在当前的运动理论和方程式上。
- 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。
- 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。