TY - GEN
T1 - A hierarchical architecture for cooperative fault accommodation of formation flying satellites in deep space
AU - Azizi, S. M.
AU - Khorasani, K.
PY - 2009
Y1 - 2009
N2 - In this paper a new fault accommodation algorithm based on a multi-level hierarchical architecture is proposed for satellite formation flying missions. This framework introduces a high level (HL) supervisor and two recovery modules: low level fault recovery (LLFR) and formation level fault recovery (FLFR). In the LLFR module, conventional recovery controller (RC) is implemented using fault severity estimation techniques. Due to imprecise fault estimation and the resulting ineffective recovery controller, the HL supervisor alerts violation of error bounds that are imposed by the mission specifications. The FLFR module is activated to compensate for the performance degradation of the faulty satellite by requiring the healthy satellites to allocate additional resources. Consequently, fault is cooperatively recovered by our proposed architecture, and the formation flying mission specifications are satisfied. Simulation results confirm the validity and effectiveness of our analytical work.
AB - In this paper a new fault accommodation algorithm based on a multi-level hierarchical architecture is proposed for satellite formation flying missions. This framework introduces a high level (HL) supervisor and two recovery modules: low level fault recovery (LLFR) and formation level fault recovery (FLFR). In the LLFR module, conventional recovery controller (RC) is implemented using fault severity estimation techniques. Due to imprecise fault estimation and the resulting ineffective recovery controller, the HL supervisor alerts violation of error bounds that are imposed by the mission specifications. The FLFR module is activated to compensate for the performance degradation of the faulty satellite by requiring the healthy satellites to allocate additional resources. Consequently, fault is cooperatively recovered by our proposed architecture, and the formation flying mission specifications are satisfied. Simulation results confirm the validity and effectiveness of our analytical work.
UR - http://www.scopus.com/inward/record.url?scp=70449644502&partnerID=8YFLogxK
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U2 - 10.1109/ACC.2009.5160190
DO - 10.1109/ACC.2009.5160190
M3 - Conference contribution
AN - SCOPUS:70449644502
SN - 9781424445240
T3 - Proceedings of the American Control Conference
SP - 4178
EP - 4183
BT - 2009 American Control Conference, ACC 2009
T2 - 2009 American Control Conference, ACC 2009
Y2 - 10 June 2009 through 12 June 2009
ER -