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In a virtual satellite, communications between any two spacecraft modules may be established on weak wireless inter-satellite using limited resources. The challenges for the attitude determination and control module include maintaining the performance with large data loss and time delay, limited on-board computational resources and hard constraints due to the limited torques that can be provided by...
This paper is concerned with application of standard wireless COTS protocols to space. Suitability of commercially available wireless sensor mote kits for communication inside and between satellites is investigated. Spacecraft applications of motes are being considered and a set of requirements are identified. Selected mote kits are tested under various scenarios complying with spacecraft testing...
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