Autonomous Mission Planning for Spin-Stabilized Science Satellites

When reducing the operations costs of a satellite program, planning and scheduling are prime areas for consideration. In particular, scheduling satellite activities is repetitive, time-consuming, and nontrivial. Automating these tasks can reduce operator staffing requirements and increase the utility of the satellite. Additionally, since the main cost of an automated scheduler is its development, being able to use the scheduler for different satellite programs would lead to great cost savings. Since there is such variety in satellite programs, no one scheduler can realistically be used to schedule them all. Automated schedulers can, however, be developed for "classes" of satellites that share the same fundamental characteristics. This paper describes a scheduler for a class of spin stabilized science satellites. Using a linear programming model of the mission, the value gained from the use of the instruments is optimized with respect to a given set of operational constraints. As a proof of concept, the scheduler is demonstrated in a case study. Finally, consideration of dynamic rescheduling in response to system failures is provided in an additional set of case studies.

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Publication Details

Journal
Digital Commons - USU (Utah State University)
Published
2025-08-21
DOI
https://doi.org/10.26077/x95n-5b54
Citations
2
Primary Topic
Space Satellite Systems and Control
Type
article

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article

Autonomous Mission Planning for Spin-Stabilized Science Satellites

Michael Ricard, Birgit Sauer
2 citations
Digital Commons - USU (Utah State University)
Space Satellite Systems and Control
article

Autonomous Mission Planning for Spin-Stabilized Science Satellites

Michael Ricard, Birgit Sauer
article en
2 citations

Abstract

When reducing the operations costs of a satellite program, planning and scheduling are prime areas for consideration. In particular, scheduling satellite activities is repetitive, time-consuming, and nontrivial. Automating these tasks can reduce operator staffing requirements and increase the utility of the satellite. Additionally, since the main cost of an automated scheduler is its development, being able to use the scheduler for different satellite programs would lead to great cost savings. Since there is such variety in satellite programs, no one scheduler can realistically be used to schedule them all. Automated schedulers can, however, be developed for "classes" of satellites that share the same fundamental characteristics. This paper describes a scheduler for a class of spin stabilized science satellites. Using a linear programming model of the mission, the value gained from the use of the instruments is optimized with respect to a given set of operational constraints. As a proof of concept, the scheduler is demonstrated in a case study. Finally, consideration of dynamic rescheduling in response to system failures is provided in an additional set of case studies.

Digital Commons - USU (Utah State University)
Draper Laboratory (US), Massachusetts Institute of Technology (US)
Charles Stark Draper Laboratory
Space Satellite Systems and Control
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