美 英 un.姿态估计 英汉 un. 1. 姿态估计 释义: 全部,姿态估计
Attitude EstimationBak, Thomas
第一步为forecast预测步骤,公式(23-25)以及(27);第二步为robust noise estimation鲁棒噪声估计,见公式(33)、估计协方差为: \hat R_k = \max\left(\frac{1}{N}\sum_{j=k-N+1}^k\lambda_j\nu_j(\lambda_j\nu_j)^\top - \tilde{P}_{k|k-1}^{yy},R_0\right)\tag{34}以及公式(26)。
3) attitude estimation 姿态估计 1. Spacecraft attitude estimation from vector measurements using particle filter integrated with unscented Kalman filter; 基于粒子滤波和UKF联合滤波的卫星姿态估计 2. Attitude estimation method for micro attitude estimation system based on FD; 基于FD的微小型姿态系统的...
@article{trawny2005indirect, title={Indirect Kalman filter for 3D attitude estimation}, author={Trawny, Nikolas and Roumeliotis, Stergios I}, journal={University of Minnesota, Dept. of Comp. Sci. \& Eng., Tech. Rep}, volume={2}, pages={2005}, year={2005}, publisher={Citeseer} } ...
3) attitude estimation 姿态估计 1. Spacecraft attitude estimation from vector measurements using particle filter integrated with unscented Kalman filter; 基于粒子滤波和UKF联合滤波的卫星姿态估计 2. Attitude estimation method for micro attitude estimation system based on FD; 基于FD的微小型姿态系统的...
This paper presents an attitude estimation system for an autonomous ground vehicle which is based on the cooperation of low-cost inertial sensors. The attitude is obtained using two different methods. The first method is based on accelerometric measurements of gravity. The second one proceeds by in...
In this paper, a sigma-point Kalman filter formulation for attitude estimation is derived using the modified Rodrigues parameters and real data of attitude... RV Garcia,DFOM Nicholas,HK Kuga,... - 《Computational & Applied Mathematics》 被引量: 6发表: 2016年 Additive Divided Difference Filtering...
MAV Attitude Estimation Using Low-Cost MEMS Inertial Sensors and GPS "Micro aerial vehicles are used primarily for surveillance and reconnaissance purposes. Especially VTOL-MAVs require permanent attitude control to be airborne. Due to constraints in weight, processing power and size, the necessary navi...
《预订 按需印刷 Fault Tolerant Attitude Estimation for Small Satellites》,作者:预订 按需印刷 Fault Tolerant Attitude Estimation for Small SatellitesChingiz Hajiyev; Halil Ersin Soken 著,出版社:taylor,ISBN:9780367689407。