搜索资源列表
spacetools
- Spacecraft Engineering Toolbox Ver. 3.2
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.
Orbital_compute
- 进行航天器轨道运算经常用到的函数，包括坐标转换，经纬度转换，二体运动，轨道要素计算-For spacecraft orbit operations frequently used functions, including coordinate conversion, latitude and longitude conversion, two-body movement, and so calculated orbital elements
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
Optimization
- 对于卫星编队飞行低推力构型重构机动的优化设计-Optimization of Low-Thrust Reconfiguration Maneuvers for Spacecraft Flying in Formation
Relative-Dynamics
- 椭圆轨道下卫星编队飞行相对运动动力学和控制-Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits
atmospheric_descent
- 用于地月轨道返回航天器轨道仿真，包括仿真主程序和大气模型-Back for the Earth-Moon orbit spacecraft orbit simulation, including the main program and the atmospheric model simulation
model_satellite
- the code of rigid spacecraft model-the code of rigid spacecraft model
CAD
- 航天器仿真与CAD 课件及程序源代码 敏感器仿真源代码-Spacecraft simulation and CAD courseware and sensor simulation program source code source code
spcacecraft
- 高斯方法求解绕地球飞行的航天器的两时刻状态变化-Gauss method for solving the spacecraft around the Earth flying two-time state change
cassiniMGA
- 卡西尼号航天器从地球飞往土星的飞行过程，卡西尼多次向大行星借力的优化程序-Cassini spacecraft to Saturn Earth during the flight, optimization program of Cassini multiple gravity assist
MGA_1DSM
- 美国航空航天局发射的探测太阳系的航天器轨道优化程序，带有深空机动-NASA solar probe launched spacecraft trajectory optimization program, with a deep space maneuver
hubulvbo
- 基于四元数互补滤波的四轴飞行器姿态解算算法。包括四元数、互补滤波、姿态结算-Solver algorithm based on quaternion complementary filter axis spacecraft attitude. Including quaternion complementary filter, posture settlement
tmg
- Tmg航天器软件数据分析软件，基于excel VBA，工程密码-Tmg spacecraft software data analysis software, based on excel VBA, engineering code 1111
C-W
- 使用CW方程，使用最小能量，采用脉冲推力，实现在一天内两航天器的交会对接。本质上就是一个交会轨道优化问题，由给定的条件优化选取设计变量，使目标函数得到最优值。-Using the CW equation, use the minimum energy, the use of pulse thrust, to achieve in a day two spacecraft rendezvous and docking. Is essentially an intersection orbit op
LanBoTe
- 使用Lambote方程方法求解在一天内两航天器的交会对接问题。最终求解冲量的最优值。-Use the Lambote equation method to solve the intersection of two spacecraft in one day. Finally, the optimal value of the impulse is solved.
Attitude-Dynamics-
- 航天动力学的一个分支，研究航天器的姿态运动，包括航天器整体围绕其质心的运动以及航天器各部分之间的相对运动-A branch of space dynamics that studies the spacecraft s attitude movement, including the motion of the spacecraft as a whole around its centroids and the relative movement between the various part
orbit
- 地月系统中，探月航天器运动的简单的数学模型，月球绕地运动近似为匀速圆周运动，程序中各天体坐标可以在JPL的星历表中查询修改。(In the Earth Moon system, the simple mathematical model of lunar exploration spacecraft motion is similar to the uniform motion around the moon. The coordinates of celestial bodies can be
用四元数为航天器设计的自适应滑模控制
- 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)