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
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