Search - 航天器姿态控制

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[Software Engineering] attitudecontrolofaircraft DL : 2: 本文首先建立了航天器姿态动力学及运动学方程，该方程具有较强的非线性特性。通过将状态耦合部分作系统干扰项的处理，使原来的非线性模型转化为线性模型加非线性干扰的形式，从而得到了更加简单明了的姿态控制系统的表达式。在应用滑模变结构原理对系统进行控制器设计时，首先通过二次型最优法求出了最优滑动面，在此基础上，利用自适应滑模控制原理，设计出了合适的系统控制律。最后，运用所设计的姿态控制系统对某航天器进行数值仿真，并对仿真结果进行了分析。仿真结果很好地体现出所设计的变结构控制器的优点，并成功地对该航天器姿态进行了控制。 -paper first established the spacecraft attitude dynamics and kinematics equation, the equation has strong nonlinear characteristics. By coupling part of the state system for the disturbance, so the original nonlinear model into a linear model nonlinear increases in the form of interference, and thus a more straightforward attitude control system expression. The application SMVSC tenets of the system controller design, the first through the quadratic optimal method, the optimal sliding surface, on this basis, using adaptive sliding control theory and design a suitable system control law. Finally, using the design of the attitude control system for a spacecraft numerical simulation, and simulation results are analyzed. Simulation results reflect good design of variable structure controller,
Date : 2008-10-13 Size : 303.69kb User : 跃进
[Other] SpacecraftAttitudeDynamicsanControl DL : 1: Spacecraft Attitude Dynamics and Control 航天器姿态控制的课件，十分难得；内容通俗易懂；十分完整；是从事航天研究的必须知识
Date : 2008-10-13 Size : 3.57mb User : 临风
[Algorithm] 小推力器姿态控制卫星控制仿真 DL : 1: Date : 2011-01-14 Size : 772byte User : wanghaibin666@qq.com
[matlab] 基于PWM的卫星喷气姿态控制系统 DL : 7: 基于刚体三轴稳定对地定向航天器的PD+PWM姿态稳定与机动仿真。在原点小偏差线性化后，经过简单计算和调试，最后确定：Kp = [700 700 900],Kd = [2330 2400 3030]，姿态运动学和姿态动力学均由m文件编写，其余由simulink基本模块搭成。压缩包里的其他文件包括PWM的测试、触发器测试和内嵌m文件。主程序为kinematics.mdl
Date : 2011-05-03 Size : 643.45kb User : springsunjyjlvzcy@126.com
[Other] SpacecraftAttitudeDynamicsanControl DL : 1: Spacecraft Attitude Dynamics and Control 航天器姿态控制的课件，十分难得；内容通俗易懂；十分完整；是从事航天研究的必须知识-Spacecraft Attitude Dynamics and Control of Spacecraft Attitude Control courseware, very rare the content of user-friendly very integrity is engaged in space research must be knowledge
Date : 2025-07-06 Size : 3.57mb User : 临风
[transportation applications] PID DL : 0: 航天器姿态控制PID控制仿真程序，加入干扰值。-PID control of spacecraft attitude control simulation program, by adding the value of interference.
Date : 2025-07-06 Size : 1kb User : eric
[Other] chapter7 DL : 0: 姿态控制部分国防科技大学航天器设计第7章-a
Date : 2025-07-06 Size : 4.44mb User : 王天祥
[matlab] Attitud6.5 DL : 3: 航天器姿态自由运动以及PID控制simulink仿真-Freedom of movement and spacecraft attitude control simulink simulation PID
Date : 2025-07-06 Size : 223kb User : 江枫
[Mathimatics-Numerical algorithms] 1xy7z.ZIP DL : 0: 挠性航天器姿态机动和振动抑制的自适应控制Flexible spacecraft attitude maneuver and vibration control adaptive control-Flexible spacecraft attitude maneuver and vibration control adaptive control
Date : 2025-07-06 Size : 511kb User : mp33
[Mathimatics-Numerical algorithms] t6u3vw.ZIP DL : 0: 带零动量轮航天器的逆系统方法姿态控制With a spacecraft attitude control based on inverse system-With a spacecraft attitude control based on inverse system
Date : 2025-07-06 Size : 596kb User : king121
[matlab] Missile-Attitude-control DL : 2: 1、利用simulink中sfunction方法建立航天器姿态动力学模型和运动学模型； 2、利用linmod对非线性模型线性化； 3、姿态模型线性化后，利用极点配置（pole）方法求取控制参数； 4、将控制参数带入非线性模型仿真控制效果。-One using simulink sfunction method to establish the dynamic model and kinematic model of the spacecraft attitude 2, the use of linmod linearization of the nonlinear model Attitude model linearization, the use of pole configuration (pole) is used to obtain the control parameters 4, the control parameters into the nonlinear model simulation control effect.
Date : 2025-07-06 Size : 9kb User : 战斗机
[Documents] speed-control- DL : 0: 采用变速控制力矩陀螺的航天器自适应姿态跟踪和稳定控制研究-Using variable speed control moment gyros Spacecraft Adaptive Attitude Tracking Study and stability control
Date : 2025-07-06 Size : 320kb User : 王德杰
[Windows Develop] speed-control- DL : 0: 采用变速控制力矩陀螺的航天器自适应姿态跟踪和稳定控制研究，编程学习源码，很好的学习资料。-With variable speed control moment gyros Adaptive Spacecraft Attitude Tracking Study and stability control, programming, learning code, good learning materials.
Date : 2025-07-06 Size : 322kb User : 孙国
[matlab] sliding-mode-method DL : 0: 航天器简化模型3D刚体摆滑模控制角速度姿态仿真程序-The attitude control of a 3D rigid pendulum with sliding mode method
Date : 2025-07-06 Size : 3kb User : 田鑫
[matlab] Rodriguez-daoli DL : 0: 航天器姿态倒立的罗德里格斯函数的建立，能够以罗德里格斯函数对航天器的姿态进行控制-Rodriguez established spacecraft attitude inverted function, it is possible to Rodriguez function spacecraft attitude control
Date : 2025-07-06 Size : 2kb User : 刁兆江
[matlab] dynamic_control DL : 0: 基于三轴航天器的姿态控制，按照实际情况，充分考虑了三轴的动力学和运动学耦合，能够单独控制各个角度姿态-Based on three-axis attitude control of the spacecraft, according to the actual situation, fully taking into account the dynamic and kinematic coupling triaxial, can be controlled separately for each angular pose
Date : 2025-07-06 Size : 11kb User : 王达从
[Applications] 用四元数为航天器设计的自适应滑模控制 DL : 2: 使用姿态四元数为航天器姿态控制设计的自适应滑模控制器(Adaptive sliding mode control for spacecraft design using quaternion)
Date : 2025-07-06 Size : 37kb User : xyzyx1995
[matlab] 粒子群优化算法 DL : 1: 用粒子群优化算法对三轴稳定航天器姿态控制PD参数进行自动寻优(optimization of PD parameter of attitude controller in spacecraft)
Date : 2025-07-06 Size : 15.45mb User : rookie Jack
[matlab] MATLAB航天姿态控制仿真程序 DL : 1: 航天器姿态控制仿真程序，利用simulink中sfunction方法建立航天器姿态动力学模型和运动学模型，利用linmod对非线性模型线性化。(The simulation program of spacecraft attitude control uses the sfunction method of Simulink to establish the dynamic model and kinematic model of spacecraft attitude, and uses limod to linearize the nonlinear model.)
Date : 2025-07-06 Size : 8kb User : woyaokaobo
[matlab] mohu DL : 0: 使用模糊PD控制对于具有初始误差的航天器姿态进行整定(Fuzzy PD control of spacecraft attitude)
Date : 2025-07-06 Size : 26kb User : 三环18

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