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Description: 本源程序是模拟飞船着陆的游戏，有一定的趣味行~！-the source of the spacecraft landing simulation of the game, have a fun trip ~!
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Size: 13312 |
Author: 小顽童 |
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Description: Spacecraft Engineering Toolbox Ver. 3.2
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Size: 322560 |
Author: 文天祥 |
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Description: 基于空间飞行器的姿态仿真源程序，仿真表明非常的准确。-Based on the spacecraft attitude simulation source code, simulation shows that very accurate.
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Size: 1024 |
Author: li |
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Description: SPACECRAFT ATTITUDE DETERMINATION BY ADAPTIVE KALMAN FILTERING
介绍了一种基于自适应卡尔曼滤波的方法-SPACECRAFT ATTITUDE DETERMINATION BY ADAPTIVE KALMAN FILTERING introduced an approach based on adaptive Kalman filtering method
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Size: 209920 |
Author: yueyang |
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Description: Particle Filtering for Sequential Spacecraft Attitude Estimation
卫星姿态估计的另外一种粒子滤波的介绍-Particle Filtering for Sequential Spacecraft Attitude Estimation for Satellite Attitude estimated another particle filter introduction
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Size: 1200128 |
Author: yueyang |
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Description: 用来计算航天器再入质点弹道，其中包括插值算法，龙格库塔法以及大气模型-Used to calculate the particle trajectory of spacecraft re-entry, including the interpolation algorithm, Runge-Kutta method as well as atmospheric model
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Size: 250880 |
Author: wang de |
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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
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Size: 3743744 |
Author: 临风 |
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Description: Spacecraft Engineering Toolbox，这个工具箱很不错的-Spacecraft Engineering Toolbox, this Toolbox is very good
Platform: |
Size: 335872 |
Author: ZhengKevin |
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Description: 基于载波相位三差的航天器GPS/INS组合姿态算法-Based on carrier phase III spacecraft poor GPS/INS Attitude Algorithm portfolio
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Size: 765952 |
Author: 陳翔 |
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Description: 二轴陀螺仪IDG300系统设计资料，可应用于空中鼠标定位，飞行器姿态校准等，该部分包含芯片的datasheet和温度补偿等方面的资料-B-axis gyroscope IDG300 system design information, can be applied to air mouse positioning, calibration, such as spacecraft attitude, which contains the chip datasheet and temperature compensation, the relevant information
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Size: 1722368 |
Author: gary xiao |
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Description: The dynamics of orbit uncertainty in an unstable orbital environment are discussed
with specific application to the orbit determination of a halo orbit about
the Earth{Sun L1 point. This article documents a simplified orbit determination
covariance program developed under Telecommunications and Mission Operations
Division Technology support. The program is ideally suited to investigate spacecraft
trajectory navigation in challenging environments, where the basic dynamics
of the trajectory can no longer be modeled using near-Keplerian motion.
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Size: 647168 |
Author: yag |
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Description: 用Directx3D开发的太阳系程序，实现了飞船在地球场景和太阳系场景的自由漫游，对于D3D的基础技术是个不错的总结-Directx3D development of the solar system with applications that implement the spacecraft in the Earth scenes and the freedom to roam the solar system scene, for D3D based technology is a good summary of
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Size: 23310336 |
Author: fytx |
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Description: _龙格_库塔_算法在航天器实时落点计算中的应用的文档。-_ Runge-Kutta _ _ real-time algorithm for spacecraft impact point calculation documents.
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Size: 273408 |
Author: sss |
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Description: 用于航天器和卫星的任务分析的早期规划，戈达德航天中心研发，源代码开放-for spacecraft mission analysis
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Size: 3026944 |
Author: chenzhi |
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Description: The ballistic category of atmospheric vehicles includes missiles, launch ve-
hicles, and entry capsules. Some missiles and launch vehicles incorporate fi ns
as aerodynamic stabilizing and control surfaces. The spacecraft are also catego-
rized according to their missions, such as low-earth orbit, medium-earth orbit,
geosynchronous orbit , lunar, and interplanetary spacecraft. Each mission is
defi ned by the payload, and orbital elements of the fi nal orbit. Of course, a
reusable launch vehicle, such as the space shuttle, is also a spacecraft with a
unique mission. -The ballistic category of atmospheric vehicles includes missiles, launch ve-
hicles, and entry capsules. Some missiles and launch vehicles incorporate fi ns
as aerodynamic stabilizing and control surfaces. The spacecraft are also catego-
rized according to their missions, such as low-earth orbit, medium-earth orbit,
geosynchronous orbit , lunar, and interplanetary spacecraft. Each mission is
defi ned by the payload, and orbital elements of the fi nal orbit. Of course, a
reusable launch vehicle, such as the space shuttle, is also a spacecraft with a
unique mission.
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Size: 7983104 |
Author: kalaiarasan.R |
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Description: 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
Platform: |
Size: 18432 |
Author: 李鑫 |
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Description: 用LabVIEW实现的“飞行姿态控制仿真”。内有vi：俯仰和滚转控制器、航向控制器、键按下增大、键盘操作、姿态角误差转换、阻尼器。还有9个显示vi和12个模型vi。
飞行控制的目的主要是通过控制飞行器的姿态和轨迹来完成飞行任务，然而飞行轨迹很大程度由飞行姿态决定。可见飞行器姿态控制，在整个飞行控制系统中处于重中之重的地位。飞行姿态控制的好坏直接关系到飞机能否安全、平稳、快速的地飞行。与其它控制系统一样，可用稳定性和动稳态性能来衡量控制效果。稳态时，要使飞行器姿态足够接近所需的飞行姿态，才能让飞机以一定的航迹航行。而姿态变化的过程，要求系统稳定，响应快，超调小，振荡少，即姿态能够快速平稳过渡。早期，可以通过优化飞机的气动布局来改良飞机的飞行性能，但随着飞行的速度与高度的增加，空气变得稀薄，阻尼随之减小，飞行的气动模型也发生了大的改变，已经难以通过外形设计来增强稳定性，而设计优良飞行姿态控制器是必由之路.
-Using LabVIEW to achieve the "flight attitude control simulation." There vi: pitch and roll control, heading control, key press increases, keyboard operation, attitude angle error change, and the dampers. There are nine show vi and 12 model vi.
The main purpose of the flight control is by controlling the aircraft attitude and flight trajectory to complete the task, but a large degree trajectory decision by the flight attitude. Spacecraft attitude control can be seen in the flight control system in the most important position. Flight attitude control has direct bearing on whether the aircraft safe, stable, fast to the ground. And other control systems, stability and dynamic steady-state performance can be measured in control performance. Steady state, make the aircraft attitude close enough to the required flight attitude, to allow the aircraft to a certain track navigation. The attitude change process, requiring system stability, fast response, small overshoot, small oscillations,
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Size: 424960 |
Author: zhou |
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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.
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Size: 9728000 |
Author: Huy |
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Description: 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
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Size: 362496 |
Author: zhangyuedong |
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Description: 航天器GN_C系统功能行为建模与仿真平台研究Functional behavior of the spacecraft GN_C System Modeling and Simulation Platform-Functional behavior of the spacecraft GN_C System Modeling and Simulation Platform
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Size: 510976 |
Author: atoz123 |
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