TY - GEN
T1 - Distributed and cooperative estimation of formation flight of unmanned vehicles subject to faults and unreliable information
AU - Azizi, S. M.
AU - Khorasani, K.
PY - 2012
Y1 - 2012
N2 - In this paper, a novel framework for cooperative estimation of formation flight of unmanned vehicles subject to presence of actuator faults is proposed. This framework is developed based on the notion of sub-observers where within a group of sub-observers each sub-observer is estimating certain states that are conditioned on a given input, output, and state information. We model the overall estimation process by a weighted estimation (WE) digraph. By selecting an appropriate path in the weighted estimation digraph, an assigned supervisor can select and configure a set of sub-observers to successfully estimate all the system states. In presence of large disturbances, noise, and faults certain sub-observers may become invalid (or unreliable), and consequently the supervisor reconfigures the set of sub-observers by selecting a new path in the estimation digraph such that the impacts of these anomalies are confined to only the local estimators. This will prevent the propagation of the uncertainties on the estimation performance of the entire formation flight system. Simulations are conducted on a five satellite formation flight system in deep space where the results confirm the validity of our analytical work.
AB - In this paper, a novel framework for cooperative estimation of formation flight of unmanned vehicles subject to presence of actuator faults is proposed. This framework is developed based on the notion of sub-observers where within a group of sub-observers each sub-observer is estimating certain states that are conditioned on a given input, output, and state information. We model the overall estimation process by a weighted estimation (WE) digraph. By selecting an appropriate path in the weighted estimation digraph, an assigned supervisor can select and configure a set of sub-observers to successfully estimate all the system states. In presence of large disturbances, noise, and faults certain sub-observers may become invalid (or unreliable), and consequently the supervisor reconfigures the set of sub-observers by selecting a new path in the estimation digraph such that the impacts of these anomalies are confined to only the local estimators. This will prevent the propagation of the uncertainties on the estimation performance of the entire formation flight system. Simulations are conducted on a five satellite formation flight system in deep space where the results confirm the validity of our analytical work.
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U2 - 10.1109/acc.2012.6314631
DO - 10.1109/acc.2012.6314631
M3 - Conference contribution
AN - SCOPUS:84869383965
SN - 9781457710957
T3 - Proceedings of the American Control Conference
SP - 3303
EP - 3308
BT - 2012 American Control Conference, ACC 2012
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2012 American Control Conference, ACC 2012
Y2 - 27 June 2012 through 29 June 2012
ER -