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attitudecontrolofaircraft
- 本文首先建立了航天器姿态动力学及运动学方程，该方程具有较强的非线性特性。通过将状态耦合部分作系统干扰项的处理，使原来的非线性模型转化为线性模型加非线性干扰的形式，从而得到了更加简单明了的姿态控制系统的表达式。 在应用滑模变结构原理对系统进行控制器设计时，首先通过二次型最优法求出了最优滑动面，在此基础上，利用自适应滑模控制原理，设计出了合适的系统控制律。 最后，运用所设计的姿态控制系统对某航天器进行数值仿真，并对仿真结果进行了分析。仿真结果很好地体现出所设计的变结构控制器的优点，并成功地
modeling_emulation
- 人体生理系统的建模与仿真在我国航天工程中的应用，神舟5号上天以前上天的飞船中“模拟人”的情况-physiological system modeling and simulation in China's space program, the application Shenzhou 5 into space before launching the spacecraft in the "simulation" of
粒子滤波的介绍
- 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
2007081312413982768
- 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
TDAPR_oddyn
- 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
ApplicationoftheRunge2KuttaAlgorithminReal2time.ra
- _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.
SpaceFlightDynamics
- 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-
Virtuasign
- 航天器电性能虚拟测试系统设计Virtual test the electrical properties of the spacecraft system design-Virtual test the electrical properties of the spacecraft system design
Integracecraft
- 航天器综合测试系统设计Integrated Test System for Spacecraft-Integrated Test System for Spacecraft
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 that can only be observed ind
guidaoxue
- 航天器轨道动力学与控制课件，1、2、3章-Spacecraft orbit dynamics and control courseware
guidao
- 航天器二体轨道动力学模型，matlab程序，simulink模型-Spacecraft orbital dynamics model of the two-body
kalman_DanSimon
- 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
spaceCraft
- 介绍单臂式空间机械臂设计中的关键技术，很具有参考价值-very good
Plasma-Sheath-Channel
- 这篇文章主要讲述了等离子鞘套的信道特征，包括电子密度的分布还有以此关于天线位置的安装等问题，得出结论可以建模为快衰落的莱斯信道，对于临近空间飞行器的通信问题提供了理论依据，但鞘套内部通信特征还是一大问题-This article describes the plasma sheath channel characteristics, including the distribution of electron density and thus the installation of the an
speed-control-
- 采用变速控制力矩陀螺的航天器自适应姿态跟踪和稳定控制研究-Using variable speed control moment gyros Spacecraft Adaptive Attitude Tracking Study and stability control
missile
- In this paper, formation control ideas for multiple spacecraft using the virtual structure approach are presented. If there is no formation feedback from the spacecraft to the virtual structure, the spacecraft will get out of formation when the v
spascraft
- In this paper, formation control ideas for multiple spacecraft using the virtual structure approach are presented. If there is no formation feedback from the spacecraft to the virtual structure, the spacecraft will get out of formation when the v
Choas-SC-Attitude-Dynamics
- Choas in Spacecraft Attitude Dynamics
Four-axis-spacecraft
- 四轴飞行器姿态控制系统设计 四轴飞行器具有不稳定、非线性、强耦合等特性,姿态控制是四轴飞行器飞行控制系统的核心 通过分析四轴飞行器的飞行 原理,根据其数学模型和系统的功能要求,设计了四轴飞行器的姿态控制系统 该系统采用stm32系列32位处理器作为主控制器,使用 ADIS16355惯性测量单元等传感器用于姿态信息检测 系统基于模块化设计的思想,各传感器都使用数字接口进行数据交换,结构简 单 使用PID控制算法进行姿态角的闭环控制,实验结果表明,飞行器能较好的稳定在实验平台上,系统