Title :
HERCULES attitude processor: gyro data processing system for real-time geolocation of images captured by astronauts
Author :
Higgins, R.F., Jr. ; Tront, J.G.
Author_Institution :
Naval Res. Lab., US Naval Center for Space Technol., Washington, DC, USA
fDate :
Jan. 31 1993-Feb. 5 1993
Abstract :
The HERCULES (hand held, earth oriented, real-time, cooperative, user friendly, location, targeting, and environmental system) attitude processor (HAP), a microprocessor-based gyro attitude data processing system used in the geolocation process, is described. The HAP software and hardware structures are discussed. A worst-case analysis of the design shows that there are no design flaws. The HERCULES HAP and attitude reference unit (ARU) are able to track the Earth rate to within 0.005 degrees per hour in some cases, and always within 0.05 degrees per hour. ARU alignment methods have been verified. Typical alignment errors are less than 0.03 degrees.<>
Keywords :
aerospace computing; aerospace instrumentation; attitude control; gyroscopes; image processing; image processing equipment; microcomputer applications; HERCULES attitude processor; alignment errors; astronauts; attitude reference unit; gyro attitude data processing; hardware; microprocessor; real-time geolocation of images; software; worst-case analysis; Cameras; Data processing; Earth; Hardware; Laboratories; Performance evaluation; Real time systems; Software performance; Space shuttles; Space technology;
Conference_Titel :
Aerospace Applications Conference, 1993. Digest., 1993 IEEE
Conference_Location :
Steamboat, CO, USA
Print_ISBN :
0-7803-0980-4
DOI :
10.1109/AERO.1993.255325
