The generalized Wahba problem

MD Shuster - The Journal of the Astronautical Sciences, 2006 - Springer
Abstract The Generalized Wahba Problem, which can accept as input both measured
directions and measured attitudes, is defined and examined in terms of both the attitude …

[PDF][PDF] Robustness and Accuracy of the QUEST Algorithm

Y Cheng, MD Shuster - Advances in the Astronautical …, 2007 - malcolmdshuster.com
A detailed study is undertaken of the accuracy and robustness of solutions to the Wahba
problem, the starting point for most modern estimators of three-axis attitude. The importance …

The TRIAD algorithm as maximum likelihood estimation

MD Shuster - The Journal of the Astronautical Sciences, 2006 - Springer
The TRIAD algorithm is shown to be derivable as a maximum-likelihood estimator. In
particular, using the QUEST measurement model, the TRIAD attitude error covariance matrix …

Integrated adaptive backstepping attitude control of spacecraft

S Soleymanpour, M Navabi - 2017 IEEE 4th International …, 2017 - ieeexplore.ieee.org
In this paper, a nonlinear adaptive backstepping Lyapunov-based controller is designed for
spacecraft. Using the Lyapunov theory, the integrated adaptive backstepping controller …

应用变速控制力矩陀螺的微小卫星大角度姿态机动控制

刘军, 韩潮 - 空间科学学报, 2007 - cjss.ac.cn
研究了变速控制力矩陀螺(VSCMG) 作为执行机构的微小卫星多目标快速姿态机动的控制问题.
控制力矩陀螺(CMG) 可以在不增加功耗, 质量和体积的条件下为微小卫星提供独特的控制力矩 …

VSCMG System Model Based on Euler Kinematics Equation

R Guan, C Li, Q Lv - Innovative Computing: Proceedings of the 4th …, 2022 - Springer
In this paper, the dynamic model of the variable speed control torque gyro (VSCMG) as a
spacecraft actuator is studied, and the VSCMG test bench device is designed. Through the …

[引用][C] Daniele Mortari

SC Design - Frontiers, 2012