Peer-to-Peer Refueling for Circular Satellite Constellations

The scheduling problem arising from refueling multiple satellites in a circular constellation is studied. It is assumed that no fuel is delivered to the constellation from an external source. Instead, all satellites in the constellation are assumed to be capable of refueling each other [peer-to-peer (P2P) refueling]. The total time to complete the rendezvous maneuvers including the refueling itself is specified. During the refueling period, each satellite may conduct a fuel exchange with at most one other satellite. Whenever two satellites perform a fuel transfer, only one is active; that is, only one of the two satellites initiates an orbital transfer to rendezvous with the inactive satellite. After the transfer of fuel is completed, the active satellite returns to its original orbital slot. The goal is to equalize the fuel among the satellites in the constellation after one refueling period while minimizing the total fuel consumed during the orbital transfers. It is shown that this problem can be formulated as a maximum-weight-matching problem on the reduced constellation graph, which can be solved using standard numerical methods. Numerical results indicate the benefits of a P2P strategy over a single-spacecraft refueling strategy for constellations with a large number of satellites.

[1]  Davoud Manouchehri,et al.  Automated resupply of consumables: Enhancement of space commercialization opportunities , 1992 .

[2]  Toru Tanabe,et al.  OTV network - New concept for the next generation space transportation system. , 1986 .

[3]  P. Tsiotras,et al.  Peer-to-peer refuelling within a satellite constellation part I: zero-cost rendezvous case , 2003, 42nd IEEE International Conference on Decision and Control (IEEE Cat. No.03CH37475).

[4]  Nicola Muscettola,et al.  Automated Planning and Scheduling for Goal-Based Autonomous Spacecraft , 1998, IEEE Intell. Syst..

[5]  Richard Studenick,et al.  Automated Fluid Interface System (AFIS) for remote satellite refueling , 1990 .

[6]  E. Distefano,et al.  Advanced Liquid Feed Experiment , 1993 .

[7]  William Hamilton.  Automatic refueling coupling for on-orbit spacecraft servicing , 1989 .

[8]  M. R. Helton.  Refurfishable satellites for low cost communications systems , 1989 .

[9]  James A. McHugh,et al.  Algorithmic Graph Theory , 1986 .

[10]  Panagiotis Tsiotras,et al.  Peer-to-peer refuelling within a satellite constellation part II: nonzero-cost rendezvous case , 2003, 42nd IEEE International Conference on Decision and Control (IEEE Cat. No.03CH37475).

[11]  G. Reinelt.  The traveling salesman: computational solutions for TSP applications , 1994 .

[12]  Panagiotis Tsiotras,et al.  Asynchronous optimal mixed P2P satellite refueling strategies , 2006 .

[13]  Barney F. Gorin.  Refueling Satellites in Space: The OSCRS Program , 1986 .

[14]  Martha E. Milton,et al.  Development and testing of the Automated Fluid Interface System , 1993 .

[15]  F. J. Hale.  Introduction to space flight , 1993 .

[16]  S. Dominick,et al.  Orbital test results of a vaned liquid acquisition device , 1994 .

[17]  Haijun Shen.  Optimal scheduling for satellite refuelling in circular orbits , 2003 .

[18]  Panagiotis Tsiotras,et al.  Optimal Scheduling for Servicing Multiple Satellites in a Circular Constellation , 2002 .

[19]  K. Alfriend,et al.  Optimal Servicing of Geosynchronous Satellites , 2002 .

[20]  Joseph H. Saleh,et al.  Space Systems Flexibility Provided by On-Orbit Servicing: Part 2 , 2002 .

[21]  Muriel Richard,et al.  Manned mission to Mars with periodic refueling from electrically propelled tankers , 1992 .

[22]  Glenn Reeves,et al.  Software architecture themes in JPL's Mission Data System , 1999, 2000 IEEE Aerospace Conference. Proceedings (Cat. No.00TH8484).

[23]  Michael Obersteiner,et al.  Orbital transfer systems for lunar missions , 1992 .

[24]  Jack Edmonds,et al.  Matching: A Well-Solved Class of Integer Linear Programs , 2001, Combinatorial Optimization.

[25]  Mitchell R. Johnson.  On-Orbit Spacecraft Re-Fluiding. , 1998 .

[26]  Sam M. Dominick,et al.  Fluid Acquisition and Resupply Experiment (FARE-I) flight results , 1993 .

[27]  Panagiotis Tsiotras,et al.  Optimal Two-Impulse Rendezvous Using Multiple-Revolution Lambert Solutions , 2003 .