Description: 针对卫星姿态控制中的一些常见运算的源码。如，四元素与欧拉角的互换，矩阵之间的运算等-against satellite attitude control of the operation some common source. For example, four elements and Euler angle swap between the matrix, etc. Platform: |
Size: 2048 |
Author:黄海滨 |
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Description: 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 Platform: |
Size: 3743744 |
Author:临风 |
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Description: 飞行器纵向回路姿态控制系统中阶跃干扰时定高平飞-Aircraft vertical loop attitude control system in step interference Gaoping set to fly Platform: |
Size: 8192 |
Author:duhaitao |
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Description: This project will use the Arduino Diecimila as the hardware platform to control a quadrocopter. Software coding will be done in the Arduino environment. The primary goal for this quadrocopter will be to create a low cost flying vehicle which integrates gyros, accelerometers and a GPS for attitude control compatible with a 2.4GHz RC controller like the Spektrum DX7. A secondary goal would be to make this an autonomous UAV, which can fly to programmed waypoints without pilot intervention. Platform: |
Size: 53248 |
Author:marshallab |
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Description: 针对三轴稳定卫星的姿态控制系统,在离散事件仿真平台OMNeT ++的
基础上,建立了一个以星敏感器和陀螺为敏感器,反作用飞轮为执行机构的闭环
控制仿真系统。采用双矢量定姿算法和P ID控制算法,对该卫星在对地定向模
式下的控制精度进行了仿真。仿真结果清晰地反映了星敏感器和反作用飞轮输
出延时对控制精度的影响。整个仿真系统符合面向对象和模块化的程序设计理
念,并实现了仿真程序的重用。-For the three-axis stabilized satellite attitude control system, discrete event simulation platform for OMNeT++ based on the establishment of a star tracker and gyro for the sensor, Reaction Wheel for the implementation of closed-loop control simulation system bodies. Dual-vector attitude determination algorithm and P ID control algorithm, the satellite-to-ground directional mode, the control precision of the simulation. The simulation results clearly reflect the star tracker and reaction flywheel output delay on the control precision effects. Consistent with the simulation system and modular object-oriented programming concepts, and realize the reuse of the simulation program. Platform: |
Size: 460800 |
Author:little |
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Description: 简介卫星姿态控制系统的模型，并针对该模型分析故障发生的特点，故
障诊断的难点，以及可能发生故障的部位和故障的类型，给出故障检测的方法。-Introduction of satellite attitude control system model and the model for the analysis of the characteristics of faults, fault diagnosis of the difficulties, and possible failure location and fault type, fault detection methods are given. Platform: |
Size: 9013248 |
Author:姜磺 |
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Description: The Spacecraft Control Toolbox is composed of MATLAB m-fi les and mat-fi les, organized into a set of modules by subject. It is essentially a library of functions for analyzing spacecraft and missions. There is a substantial set of
software which the Spacecraft Control Toolbox shares with the Aircraft Control Toolbox, and this software is in a module called Common. The core spacecraft fi les are in SC and SCPro along with special plotting tools in Plotting.
The new CubeSat module demonstrates mission planning and simulation for nanosatellites. These fi ve modules are referred to together as the Core toolbox. Functions for estimation, orbit analysis, subsystem analysis, and detailed
attitude control system examples are grouped in separate modules. All of the modules are described in the following table, including the add-on modules which are purchased separately. Platform: |
Size: 9728000 |
Author:Huy |
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Description: 通过姿态控制改变卫星面质比的优化算法研究Satellite attitude control by changing the surface quality of the optimization algorithm than-Satellite attitude control by changing the surface quality of the optimization algorithm than Platform: |
Size: 174080 |
Author:atoz123 |
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Description: simulate multivariable system control.
Attitude Control of Spinning Satellite Subject to Actuators
Restriction Using EigenStructure Assignment.
Platform: |
Size: 2350080 |
Author:hasan |
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Description: 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. Platform: |
Size: 9216 |
Author:战斗机 |
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Description: 研究卫星姿控系统快速建模问题，根据姿态控制原理以及控制系统的基本结构,提出建立了三轴稳定卫星姿态控制系统仿真通用模块库，并通过一个仿真算例验证了模块库的有效性。-Research Satellite Attitude Control System rapid modeling problem, proposed the establishment of a three-axis stabilized satellite attitude control system simulation Universal module library, and through a simulation example of the effectiveness of the module library. Platform: |
Size: 699392 |
Author:叶新 |
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Description: 利用STK中读姿态外部数据的方式实现的飞船返回调姿过程。-Procedure of attitude control of spaceship when return by external attitude data in STK. Platform: |
Size: 2501632 |
Author:刘世勇 |
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Description: 自动控制理论中卫星姿态控制系统，利用MATLAB画出已校正系统的单位阶跃和单位斜坡响应曲线。-The satellite attitude control system of automatic control theory is used to draw the unit step and slope response curve of the corrected system with MATLAB. Platform: |
Size: 240640 |
Author:李冠楠 |
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