Technical Papers
Sep 26, 2018

Energy-Dependent Mission Planning for Agile Earth Observation Satellite

Publication: Journal of Aerospace Engineering
Volume 32, Issue 1

Abstract

This paper investigates the energy-dependent mission planning of an agile earth observation satellite. According to the similarities between energy-dependent mission planning and the dynamic traveling salesman problem (DTSP), the energy-dependent mission planning is converted into a DTSP through two mappings from observation angle and energy to city and distance. In addition, to eliminate the uncertainty of feasible attitude trajectories/energy for a given scheduling strategy, a multiple-stage optimal energy factor is developed for the model extension. The paper further uses the time-optimal minΔTtransi1,i in the transition time constraint as an input of the model to enlarge the optional execution time for the subsequent target in a consecutive observation. To solve this problem, a hybrid method integrating the Gauss pseudospectral method and the genetic algorithm (GPM-GA) is proposed which uses the genetic algorithm to generate the feasible solutions for scheduling process, whereas the Gauss pseudospectral method (GPM) is used to optimize the energy and the transition time constraint parameter for each solution. Extensive simulation results show that, compared with the classical genetic algorithm (CGA), the energy consumption and simulation time of the proposed algorithm are decreased effectively. In particular, the simulation time decreases more obviously with larger target sizes. Furthermore, attitude trajectory projections of satellite motion provided by GPM-GA are much smoother. These numerical and visualization results demonstrate the superiority of GPM-GA in terms of energy efficiency, computational efficiency, and attitude trajectory smoothing.

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Acknowledgments

The authors thank the editor and anonymous reviewers for their helpful comments and suggestions. This work was supported by the National Natural Science Foundation of China (Grant No. 61633008), the National Natural Science Foundation of Heilongjiang Province (Grant No. F2017005), the Fundamental Research Fund for the Central University of Harbin Engineering University (Grant No. HEUCFP201768), the Postdoctoral Scientific Research Developmental Heilongjiang Province of China (Grant No. LBH-Q14054), and the China Scholarship Council Foundation.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 32Issue 1January 2019

History

Received: Nov 7, 2017
Accepted: Jun 14, 2018
Published online: Sep 26, 2018
Published in print: Jan 1, 2019
Discussion open until: Feb 26, 2019

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Professor, College of Automation, Harbin Engineering Univ., Harbin 150001, China. Email: [email protected]
Ph.D. Student, College of Automation, Harbin Engineering Univ., Harbin 150001, China. Email: [email protected]
Assistant Professor, College of Automation, Harbin Engineering Univ., Harbin 150001, China (corresponding author). Email: [email protected]
Ph.D. Student, College of Automation, Harbin Engineering Univ., Harbin 150001, China. Email: [email protected]

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