Development of a hardware simulator for the attitude estimation of a spacecraft on the ground test
Author:
Affiliation:
1. Osaka Institute of Technology,Dept. of Electrical and Electronic Systems Engineering,Osaka,Japan
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9905734/9905735/09905782.pdf?arnumber=9905782
Reference16 articles.
1. Nonlinear filtering for sequential spacecraft attitude estimation with real data: Cubature Kalman Filter, Unscented Kalman Filter and Extended Kalman Filter
2. A study on attitude motion estimation of a decommissioned spacecraft with visual tracking of feature points;miyazaki;Proc of the 60th Annual Conference of the Society of Instrument and Control Engineers of Japan SICE 2021,2021
3. Real-time spacecraft simulation and hardware-in-the-loop testing
4. Hardware-in-the-Loop, Three-Axis Simulator of Spacecraft Attitude Maneuvering with Nanosatellite Dimensions;chesi;Journal Of Small Satellites,2015
5. Design Standard Mechanisms;JREG-2 - 330,2009
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