搜索资源列表
Matlabtoolbox_space
- Matlab航天器工具箱，用于轨道计算，2D或3D的平面显示，包含计算多卫星轨道动力学模型和地面覆盖分析等-Matlab toolbox spacecraft for orbit calculation, 2D or 3D graphic display, including the calculation of multi-satellite orbital dynamics analysis model and floor coverings
Spacecraft_Engineering_Toolbox
- Spacecraft Engineering Toolbox，这个工具箱很不错的-Spacecraft Engineering Toolbox, this Toolbox is very good
LowThrust_Transfer
- 小推力航天器转移轨道程序，包括matlab源码和说明文档-Small thrust spacecraft transfer orbit procedures, including source and documentation matlab
Spacecraft_Control_Toolbox
- 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 softwa
atmos_space_flight
- 大气层内航天器飞行动力学matlab仿真模型-The atmosphere inside the spacecraft flight dynamics matlab simulation model
scripts
- 在一个任意的天线方向图下，利用遗传算法使其接近所给的理想天线方向图。这种方法已经在NASA和其他机构中所利用来制造航天器。这些程序是自动生成一个2.4GHz的微波天线，利用遗传算法和NEC2模拟工具，来实现优化天线。包括最初级的简单双极形天线，在这个基础上又设计了三维空间中两部分天线和三维空间中多部分天线。-In a partially random antenna layout, and use a genetic algorithm to evolve a better solution.
homeplanet
- 人类必须在最短的时间内迁往月球。现有n个太空站位于地球与月球之间，且有m 艘公共交通太空船在其间来回穿梭。每个太空站可容纳无限多的人，而每艘太空船i 只可容纳H[i]个人。每艘太空船将周期性地停靠一系列的太空站，例如：(1，3，4)表示该太空船将周期性地停靠太空站134134134…。每一艘太空船从一个太空站驶往任一太空站耗时均为1。人们只能在太空船停靠太空站(或月球、地球)时上、下船。初始时所有人全在地球上，太空船全在初始站。 试设计一个算法，找出让所有人尽快地全部转移到月球上的
matlab_file1
- 分布式星载干涉GMTI雷达系统仿真 performance analysis of a space-based GMTI radar system using separated spacecraft interferometry-Distributed Spaceborne Interferometric GMTI radar system simulation performance analysis of a space-based GMTI radar system using se
kepler.m
- 实现探测器的轨道的开普勒描述，是一个很好的仿真程序-TO REALIZE THE ORBIT FOR SPACECRAFT IN KAPLER
Spacduling
- 蚁群算法航天器观测动态调度Spacecraft observations ant colony algorithm Dynamic Scheduling-Spacecraft observations ant colony algorithm Dynamic Scheduling
titude
- 单球无味卡尔曼滤波在飞船姿态估计中的应用-Unscented Kalman filter in single-ball estimate of spacecraft attitude
0815109
- 分析并设计kalman滤波器，应用其对航天器得飞行状态量进行实时估计，得到较为准确的状态参量，-Kalman filter analysis and design, application of their spacecraft in real time the amount was estimated flight to get a more accurate state parameter,
thods
- 航天器故障状态诊断和上行数据验证方法Diagnosis and fault status of spacecraft uplink data validation methods-Diagnosis and fault status of spacecraft uplink data validation methods
atus
- 灰色系统理论的航天器故障状态预测方法Grey system theory prediction of spacecraft fault status-Grey system theory prediction of spacecraft fault status
Simulation
- P_FUZZY_PID飞行器大角度机动控制物理仿真-Control of Spacecraft Large Angle Maneuvers P_FUZZY_PID Physical Simulation
Attitud6.5
- 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
main-dqjs
- 线性拟合程序,航天器运算结果可以进行拟合运算-Linear fitting procedure, spacecraft operations to fit the computing results can be
spacecraft-code
- 一个航天器的动力学响应程序，采用模态价值分析准则和内平衡法则进行模型降阶。-Dynamic response of a spacecraft program, the use of value analysis mode within the balance guidelines and rules for model reduction.
spacecraft-attitude-quaternion
- 对航天器的姿态以四元数的方法建立的仿真模型 。对航天器进行建模-The simulation model for spacecraft attitude quaternion method established. Spacecraft modeling
sc_attitude-master
- Goal of this project is to simulate the rotational motion of a spacecraft in orbit. Plots of Euler angles and polhode curves (angular velocity time histories) are generated. Equations of Motion included in this package are for a rigid body in a torqu