搜索资源列表
Integracecraft
- 航天器综合测试系统设计Integrated Test System for Spacecraft-Integrated Test System for Spacecraft
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,
TSdiction
- TSEOPM在轨航天器故障预报方法研究TSEOPM spacecraft in orbit Fault prediction-TSEOPM spacecraft in orbit Fault prediction
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
AttDet
- 航天器姿态确定工具包,可利用CA码和L1载波进姿态确定 -attitude determinantion tool
Attitud6.5
- 航天器姿态*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
ant_base_cap
- 天线和航天器之间的电容计算，应用矩量法求解，航天器模型为STEREO-numarical method of computing capacitance between antenna and the spacecraft body
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.
3434
- 基于视觉信息的航天器位姿估计迭代算法.Based on visual information, spacecraft position and attitude estimation iterative algorithm.-Based on visual information, spacecraft position and attitude estimation iterative algorithm.
Methods-of-LDPC-codec
- 对LDPC编译码的发展作了分析，发表在航天器工程杂志上。-Methods of LDPC codec
kalmanfilter
- 原来被用在航天器导航，如今卡尔曼滤波器使用于许多应用程序。它主要是用来估计系统狀態只能直接观察或不准确的系统本身。-Originally developed for use in spacecraft navigation, the Kalman filter turns out to be useful for many applications. It is mainly used to estimate system states
1xy7z.ZIP
- 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
t6u3vw.ZIP
- 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
Missile-Attitude-control
- 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
GTOPtoolbox
- 这是航天器轨迹优化的程序，包括深空探测，空空导弹。-This is the optimization of the spacecraft track program, including deep space exploration, an air-to-air missile.
Spacecraft-orbit-extrapolation-code
- 航天器轨道外推代码（FORTRAN95/2003科学计算与工程，宋叶志），旨在介绍常微分方程处置问题的应用。-Spacecraft orbit extrapolation code (FORTRAN95/2003 scientific computing and engineering, Sung YE), aims to introduce the ordinary differential equation of the dispo
flight-dynamics-matlab-model
- 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
optimal_impulsive
- 最优脉冲轨道机动所需的圆形或椭圆形地球轨道的航天器。optimal impulsive maneuver required to de-orbit a spacecraft in a circular or elliptical Earth orbit-Round or oval Earth orbit spacecraft the optimal pulse orbital maneuvering required. optimal