Title :
Calibration of inductosyn cyclic error
Author_Institution :
Hughes Aircraft Co., El Segundo, CA, USA
Abstract :
A laboratory test using the Hughes´s built single-axis scan mirror demonstration unit was conducted to generate test data which were used to validate the previously developed on-orbit inductosyn cyclic error calibration concept. This paper describes the test set-up, the test data, and the calibration results. Based on the obtained results, the author believes that the technical feasibility of applying the proposed on-orbit calibration scheme to meet the 0.5 micro radian inductosyn cyclic error requirement has been demonstrated
Keywords :
aerospace control; aerospace testing; calibration; cyclic error; inductosyn; on-orbit calibration scheme; single-axis scan mirror; test set-up; Calibration; Space vehicle control; Space vehicle testing;
Conference_Titel :
Control Applications, 1994., Proceedings of the Third IEEE Conference on
Conference_Location :
Glasgow
Print_ISBN :
0-7803-1872-2
DOI :
10.1109/CCA.1994.381229
