Design of optimal observation strategy for re-entry prediction improvement of GTOs upper stage
Design of optimal observation strategy for re-entry prediction improvement of GTOs upper stage
In this paper, an automatic approach to design the observation strategy of spent upper stage moving on GTOs is presented. More specifically, the design is formulated as a multi-objective optimization problem solved by means of a multi-objective genetic algorithm (MOGA). This approach allows minimizing both the number of total measurements required to detect the object and the error on re-entry prediction. Within the optimization process a nonlinear OD algorithm is run to determine the estimates of both initial state and model parameters and the associated covariance matrix. The Nonlinear Least Square Estimator (NLSE) technique is implemented, exploiting the differential algebra framework for Jacobian matrix computation in order to reduce the computational effort related to OD problem solution. Finally, the software tool IRIS is developed to accurately simulate the observation campaign based on geometry and constraints of existing sensors currently available to the European Space Agency (ESA). Numerical simulations are performed to demonstrate the efficiency of the proposed approach.
Di Mauro, Giuseppe
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Rasotto, Mirco
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Di Lizia, Pierluigi
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Armellin, Roberto
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Funke, Quirin
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Flohrer, Tim
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15 March 2016
Di Mauro, Giuseppe
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Rasotto, Mirco
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Di Lizia, Pierluigi
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Armellin, Roberto
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Funke, Quirin
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Flohrer, Tim
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Di Mauro, Giuseppe, Rasotto, Mirco, Di Lizia, Pierluigi, Armellin, Roberto, Funke, Quirin and Flohrer, Tim
(2016)
Design of optimal observation strategy for re-entry prediction improvement of GTOs upper stage.
6th International Conference on Astrodynamics Tools and Techniques (ICATT), Darmstadt, Germany.
14 - 17 Mar 2016.
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Conference or Workshop Item
(Paper)
Abstract
In this paper, an automatic approach to design the observation strategy of spent upper stage moving on GTOs is presented. More specifically, the design is formulated as a multi-objective optimization problem solved by means of a multi-objective genetic algorithm (MOGA). This approach allows minimizing both the number of total measurements required to detect the object and the error on re-entry prediction. Within the optimization process a nonlinear OD algorithm is run to determine the estimates of both initial state and model parameters and the associated covariance matrix. The Nonlinear Least Square Estimator (NLSE) technique is implemented, exploiting the differential algebra framework for Jacobian matrix computation in order to reduce the computational effort related to OD problem solution. Finally, the software tool IRIS is developed to accurately simulate the observation campaign based on geometry and constraints of existing sensors currently available to the European Space Agency (ESA). Numerical simulations are performed to demonstrate the efficiency of the proposed approach.
Text
6th-ICATT-DESIGN OF OPTIMAL OBSERVATION STRATEGY FOR RE-ENTRY PREDICTION IMPROVEMENT OF GTOs UPPER STAGE_Update.pdf
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Published date: 15 March 2016
Venue - Dates:
6th International Conference on Astrodynamics Tools and Techniques (ICATT), Darmstadt, Germany, 2016-03-14 - 2016-03-17
Organisations:
Astronautics Group
Identifiers
Local EPrints ID: 390311
URI: http://eprints.soton.ac.uk/id/eprint/390311
PURE UUID: cfe1cc1b-b82a-4a5e-be96-923015a0d00d
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Date deposited: 23 Mar 2016 12:18
Last modified: 14 Mar 2024 23:15
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Contributors
Author:
Giuseppe Di Mauro
Author:
Mirco Rasotto
Author:
Pierluigi Di Lizia
Author:
Quirin Funke
Author:
Tim Flohrer
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