DocumentCode :
2288206
Title :
Look, ma, no HANS! [High Accuracy Navigation Systems]
Author :
Hong, Philip ; Carlisle, George ; Smith, Nicholas
Author_Institution :
Lockheed Martin Astronaut., Denver, CO, USA
Volume :
7
fYear :
2002
fDate :
2002
Firstpage :
463676
Abstract :
As part of the low cost design, the spinning Genesis spacecraft has no High Accuracy Navigation Systems (HANS) on board, such as gyros or accelerometers. All science requirements are met, although accurate pointing estimation is limited to spin rates less than 2 rpm, due to star tracker characteristics, and less than 28° off Sun, because of the two-axis Sun sensor characteristics. Payload contamination concerns result in thruster locations that produce uncoupled forces, and significant translational delta-V, whenever pointing or spin rate are changed. Nevertheless, with creative systems, mission and subsystems design, planning and operations, Genesis should exceed all science objectives. The Genesis lessons learned will benefit future mission design and operations in the areas of both planned activities and off-nominal situations.
Keywords :
aerospace computing; aerospace propulsion; artificial satellites; attitude control; navigation; Discovery class mission; low cost design; spin rate; spinning Genesis spacecraft; star tracker characteristics; thruster locations; translational delta-V; two-axis Sun sensor characteristics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1035294
Filename :
1035294
Link To Document :
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