Estimating Attitude from Vector Observations Using a Genetic Algorithm-Embedded Quaternion Particle Filter 介紹了一種基于四元數粒子濾波的方法
標簽： Algorithm-Embedded Observations Estimating Quaternion
上傳時間： 2013-12-29
上傳用戶：集美慧
SPACECRAFT Attitude DETERMINATION BY ADAPTIVE KALMAN FILTERING 介紹了一種基于自適應卡爾曼濾波的方法
標簽： DETERMINATION SPACECRAFT FILTERING Attitude
上傳時間： 2014-01-25
上傳用戶：hakim
Particle Filtering for Sequential Spacecraft Attitude Estimation 衛星姿態估計的另外一種粒子濾波的介紹
標簽： Estimation Sequential Spacecraft Filtering
上傳時間： 2014-07-06
上傳用戶：cxl274287265
digit book about Attitude on mobile
標簽： Attitude mobile digit about
上傳時間： 2016-05-05
上傳用戶：anng
Spacecraft Attitude Dynamics and Control 航天器姿態控制的課件，十分難得；內容通俗易懂；十分完整；是從事航天研究的必須知識
標簽： Spacecraft Attitude Dynamics Control
上傳時間： 2016-08-11
上傳用戶：hongmo
詳細分析了姿態估值器與四元數估值器。Attitude ESTIMATION OR QUARTERNION ESTIMATION
標簽： ESTIMATION QUARTERNION Attitude OR
上傳時間： 2016-10-07
上傳用戶：dongbaobao
satellite Attitude determination
標簽： determination satellite Attitude
上傳時間： 2014-08-08
上傳用戶：
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.
標簽： demonstration longitudinal Aerospace Grumman
上傳時間： 2016-05-17
上傳用戶：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
標簽： incorporating measurements integrated pseudolite
上傳時間： 2013-12-10
上傳用戶：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.
標簽： comprehensive principal the approach
上傳時間： 2016-10-18
上傳用戶：蠢蠢66
