4. 无迹姿态滤波器 Unscented Attitude Filter 5. 仿真示例 Simulation Example 6. 总结 Conclusions 引用 @article{crassidis2003unscented, title={Unscented filtering for spacecraft attitude estimation}, author={Crassidis, John L and Markley, F Landis}, journal={Journal of guidance, control, and dynamics...
This paper presents a new algorithm for the estimation of spacecraft attitude from vector observations. Belonging to the class of Monte Carlo sequential methods, the new estimator is a particle filter that uses approximate numerical representation techniques for performing the otherwise exact time ...
Single-Axis Attitude Determination Methods James R. Wertz Pages 362-409 Three-Axis Attitude Determination Methods James R. Wertz Pages 410-435 State Estimation Attitude Determination Methods James R. Wertz Pages 436-470 Evaluation and Use of State Estimators James R. Wertz Pages 471...
6) spacecraft attitude determination 航天器姿态测量补充资料:航天器姿态敏感器 航天器姿态控制系统的测量部件。它获取航天器的姿态信息,输出与姿态参数成函数关系的电量。按获取姿态信息的方法,姿态敏感器分为光学敏感器、惯性敏感器、射频敏感器和磁敏感器等几类。 ①光学敏感器:对某些姿态参考源(主要是天体)发出...
Kalman Filtering for Spacecraft Attitude Estimation(清晰版)D o w n l o a d e d b y B E I J I N G I N S T I T U T E O F T E C H N O L O G Y o n F e b r u a r y 27, 2014 | h t t p ://a r c .a i a a .o r g | D O I :...
5) spacecraft attitude estimation 航天器姿态估计6) Spacecraft attitude dynamics 航天器姿态动力学 1. This paper reviews some nonlinear problems in spacecraft attitude dynamics, which include attitude stability of multibody spacecraft, spacecraft with flexible bodies, and spacecraft containing liquid....
An interlaced matrix Kalman filter, which is based on vector observations and gyro measurements, is proposed for spacecraft attitude estimation in this paper. It combines the matrix Kalman filter and cubature Kalman filter to estimate spacecraft attitude and gyro drift bias, respectively. The defects...
A particle filter(PF) based algorithm is given to solve the attitude estimation problem of the three-axis stabilized based on vector observations and biased gyro.In order to avoid the potential computational burden problem associated with the number of required particles,this algorithm using a dual ...
The performance advantage of the AIEKF is illustrated via Monte Carlo simulations on a typical relative position and attitude estimation application. Through comparisons in different scenarios, the presented algorithm is shown to improve adaptability and ensure estimation accuracy.Kai Xiong...
Evaluation of a spacecraft attitude and rate estimation algorithm. International Journal of Aircraft Engineering and Aerospace Technology. 2010; 82(3): 184-193.Filipski, M.N., Varatharajoo, R.: Evaluation of a Spacecraft Attitude and Rate Estimation Algorithm. Aircraft Engineering and Aerospace ...