OPTIMAL DESIGN OF GUIDANCE ALGORITHM FOR THE RECONFIGURATION PHASE OF THE SATELLITE CONSTELLATION

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FAKOOR MAHDI; BAKHTIARI MAJID; SOLEYMANI MAHSHID

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Journal: Modares Mechanical Engineering Year:2016 | Volume:16 | Issue:2 Page(s): 31-40

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Title

OPTIMAL DESIGN OF GUIDANCE ALGORITHM FOR THE RECONFIGURATION PHASE OF THE SATELLITE CONSTELLATION

Author(s)

FAKOOR MAHDI | BAKHTIARI MAJID | SOLEYMANI MAHSHID | Issue Writer Certificate

Keywords

SATELLITE CONSTELLATIONQ1

RECONFIGURATION PHASEQ1

LAMBERT TARGETING THEOREMQ1

HYBRID PSO/GA OPTIMIZATION ALGORITHMQ1

Abstract

A novel approach is presented for the reconfiguration of SATELLITE CONSTELLATIONs based on Lambert’s theorem. The reconfiguration problem in this article, is considered with the constraint of overall fuel cost minimization. Hence, orbital maneuvers required for the operation of reconfiguration are designed in such a way that, transferring globally the satellites to the desired configuration of constellation will be possible at minimal cost. Also, the introduced method of orbital transfer for implementing the RECONFIGURATION PHASE of SATELLITE CONSTELLATION has no limitation on the shape and orientation of initial and target orbits such as: co-planarity, coaxiality, circularity and/or the existence of a common point.Moreover, a method is offered for modeling the cost function of reconfiguration problem in which the two important tasks of optimal orbital transfer of satellites to the target configuration of constellation and optimal assignment of each satellite to a specific terminal position or final orbit will be done in one single step. For this purpose and in order to achieve globally optimal solution of the reconfiguration problem of constellation the hybrid PSO/GA is used. Finally, two different scenarios of reconfiguration of SATELLITE CONSTELLATION will be modeled once by the presented approach and once by considering determined positions of flight and deployment for the satellites. The obtained results indicate the superiority of the idea presented in this article.

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APA: Copy

FAKOOR, MAHDI, BAKHTIARI, MAJID, & SOLEYMANI, MAHSHID. (2016). OPTIMAL DESIGN OF GUIDANCE ALGORITHM FOR THE RECONFIGURATION PHASE OF THE SATELLITE CONSTELLATION. MODARES MECHANICAL ENGINEERING, 16(2), 31-40. SID. https://sid.ir/paper/178818/en

Vancouver: Copy

FAKOOR MAHDI, BAKHTIARI MAJID, SOLEYMANI MAHSHID. OPTIMAL DESIGN OF GUIDANCE ALGORITHM FOR THE RECONFIGURATION PHASE OF THE SATELLITE CONSTELLATION. MODARES MECHANICAL ENGINEERING[Internet]. 2016;16(2):31-40. Available from: https://sid.ir/paper/178818/en

IEEE: Copy

MAHDI FAKOOR, MAJID BAKHTIARI, and MAHSHID SOLEYMANI, “OPTIMAL DESIGN OF GUIDANCE ALGORITHM FOR THE RECONFIGURATION PHASE OF THE SATELLITE CONSTELLATION,” MODARES MECHANICAL ENGINEERING, vol. 16, no. 2, pp. 31–40, 2016, [Online]. Available: https://sid.ir/paper/178818/en

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