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7下载：
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
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Maxwell Noton书中的程序
originally compiled and linked in Borland Turbo C++, version 3.0-SPACECRAFT NAVIGATION AND GUIDANCE
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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
covari
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GPS/INS组合导航方面的一篇学位论文，讲得还不错，有点参考价值。-Integrated GPS INS Navigation System Design for Autonomous Spacecraft Rendezvous
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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 that can only be observed ind
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用于四轴飞行器的姿态算法，内含各种矩阵加减乘转置、求逆等运算，及姿态kalman滤波算法，可适用于低速旋翼机的姿态导航-For four-axis spacecraft attitude algorithm, containing a variety of matrix addition and subtraction to multiply the transpose and inverse operations, and attitude Kalman filtering algorithm
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本程序实现星光导航中定姿算法的最小二乘算法，基于星敏感器观测星光信息，得到飞行器姿态-Program starlight navigation, attitude determination algorithm least squares algorithm, based star sensor observations Starlight information, Spacecraft Attitude
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kalman filter
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 that can only be observed indirectly or inaccurately by the
syste
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用于解决航天动力学，航天任务设计，导航制导控制问题-The Java Astrodynamics Toolkit is a library of components to help users create their own application programs to solve problems in astrodynamics, mission design, spacecraft navigation, guidance and control using Java or Matl
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