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satellite1
- 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.
PID
- 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.
satellite_orbit
- 卫星轨道方面的知识，卫星轨道姿态动力学与控制-Knowledge of satellite orbit, the satellite attitude and orbit dynamics and control
C_newtyle
- 航天常用姿态确定敏感器组合，太阳敏感器+速率陀螺+轨道罗盘，具体数据含义请参考章仁为的<《卫星姿态控制》>-Spacecraft attitude determination sensors commonly used in combination, sun sensor+ rate gyro compass+ tracks, the meaning of specific data please refer to Chapter Ren' s < " Satell
IIC
- 四轴飞行器程序，能够实现飞行器的稳定飞行，姿态控制和自旋飞行。-Four aircraft program, the aircraft can achieve a stable flight attitude control and spin in flight.
suan
- 四旋翼飞行器控制算法，主要通过控制四旋翼飞行器的姿态和位置，使得飞行器在飞行过程中能够稳定飞行。目前存在的PID控制算法，在鲁棒性、相应速度以及抗干扰方面的性能不是很好。本算法则是使用模糊PID的控制算法，能够满足四旋翼飞行器的需求。-Four-rotor control algorithms, mainly by controlling the attitude and position of the four-rotor aircraft, making the aircraft durin
sizhoufeixingqi_code
- 此代码是基于STM32飞控板的四轴飞行器代码，融合了新的姿态解析算法-This code is based on the STM32 four-axis flight control board aircraft code, integration of a new attitude resolution algorithm
wm
- 水面无人艇(Unmanned Surface Vehicle)的航迹控制对提升无人艇艇载设备 侦察观测效果以及多任务作战能力具有十分ffi要的意义。由于受到风、浪、流等 干扰环境影响,水而无人艇将产生六自由度的操纵运动,具有很强的非线性和随 机性。这将致使无人艇的航向航迹及姿态控制具有一定的难度,因此需要对水面 无人艇建立六自由度操纵模型,更好地实现对无人艇的控制。 采用经典的MMG分离建模思想,依托浜本刚实提出的水平附体坐标系,建 立
satellite-fuzzy
- 挠性卫星姿态动力学建模及模糊控制与PID控制对比-Dynamic modeling and fuzzy control of flexible satellite attitude control and PID control
PIDrigid-satellite
- 刚体卫星姿态PID控制，在有无干扰及飞轮失效情况下的仿真-PID control of rigid satellite attitude of actuator for flywheel
attitude-of-spacship-when-return
- 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.
mc_att_control_main
- 无人机的姿态控制代码，可以对无人机的姿态进行实时控制-Attitude control of unmanned aerial vehicle (uav) code, can be real-time control of unmanned aerial vehicle (uav) attitude
zitai
- 描述刚体卫星姿态稳定控制的程序。分为三种情况，小推力控制，飞轮控制与小推力飞轮联合控制。能在干扰下稳定卫星的姿态。- The program of attitude stabilization control for rigid satellite. It is divided into three situations: small thrust control, flywheel control and small thrust flywheel combined control.
Heli
- 直升机飞行控制律仿真，包含姿态及位置反馈回路，PID控制算法，及模糊控制算法(Helicopter flight control law simulation, including attitude and position feedback loop, PID control algorithm, and fuzzy control algorithm)