Estimating ATTITUDE from Vector Observations Using a Genetic Algorithm-Embedded Quaternion Particle Filter 介绍了一种基于四元数粒子滤波的方法
标签： Algorithm-Embedded Observations Estimating Quaternion
上传时间： 2013-12-29
上传用户：集美慧
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
标签： DETERMINATION SPACECRAFT FILTERING ATTITUDE
上传时间： 2014-01-25
上传用户：hakim
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
标签： Estimation Sequential Spacecraft Filtering
上传时间： 2014-07-06
上传用户：cxl274287265
digit book about ATTITUDE on mobile
标签： ATTITUDE mobile digit about
上传时间： 2016-05-05
上传用户：anng
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
标签： Spacecraft ATTITUDE Dynamics Control
上传时间： 2016-08-11
上传用户：hongmo
详细分析了姿态估值器与四元数估值器。ATTITUDE ESTIMATION OR QUARTERNION ESTIMATION
标签： ESTIMATION QUARTERNION ATTITUDE OR
上传时间： 2016-10-07
上传用户：dongbaobao
satellite ATTITUDE determination
标签： determination satellite ATTITUDE
上传时间： 2014-08-08
上传用户：
This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 Tomcat. First order linear approximations of the aircraft and actuator behavior are connected to an analog flight control design that uses the pilot s stick pitch command as the set point for the aircraft s pitch ATTITUDE and uses aircraft pitch angle and pitch rate to determine commands. A simplified Dryden wind gust model is incorporated to perturb the system.
标签： demonstration longitudinal Aerospace Grumman
上传时间： 2016-05-17
上传用户：wang5829
This paper deals with the issue of incorporating pseudolite measurements into an integrated Global Positioning System/ Inertial Navigation System ~GPS/INS! positioning and ATTITUDE system with a view to improving signal availability, solution reliability, and accuracy in a localized area
标签： incorporating measurements integrated pseudolite
上传时间： 2013-12-10
上传用户：wmwai1314
This paper provides a rigorous comprehensive approach to the design of the principal software algorithmsutilized inmodern-day strapdown inertial navigationsystems: integration of angular rate into ATTITUDE, acceleration transformation/integration into velocity, and integration of velocity into position.
标签： comprehensive principal the approach
上传时间： 2016-10-18
上传用户：蠢蠢66
