Abstract

In current Mars relay communications, the Consultative Committee for Space Data Systems (CCSDS) Proximity-1 protocol is simple and efficient but it exhibits low flexibility in optimal access orbiter selection. Once connected with the first successful hailing orbiter, the rover would not switch to other better orbiters until the end of that connection, which makes it difficult to provide more convenient and efficient data relay services. The entire system cost is essential for optimal access orbiter selection, which includes both the Proximity-1 links' transmission cost concerned with the data transmission energy consumption and the orbiters' storage cost concerned with the data buffering energy consumption, thus minimizing the system cost on unit data volume could reduce energy consumption and extend the deep space vehicle's life. We employ long-term simulations of the single rover, simultaneously tracking two orbiters utilizing the improved Hotelling oligopoly model, and reveal the potential improvements for the current “first-come first-serve” selection strategy. In this article, a complete solution is proposed to solve the optimal access orbiter selection issues, including the geometric model, orbit design, oligopoly model, storage cost, and optimal selection algorithms. Simulation results show that our new algorithm outperforms current CCSDS Proximity-1 protocols and distance-dependent selection algorithm in the system cost on unit data volume with the selection gains $36.14\%$ and $ 29.59\%$, respectively, which could be used as the rover's optimal access orbiter selection algorithm in Mars automatic relay communications.

Highlights

  • During the Mars rover exploration phase, it is necessary to send the Mars surface exploration data back to Earth for scientific research and other important applications

  • The Consultative Committee for Space Data Systems (CCSDS) has studied and recommended a series of “Proximity-1” protocols with the orbiter-mastered hailing channel and single-access working channel related to the Mars relay communications [8]

  • For Mars orbiter, it is assumed that each orbiter has the limited data storage space of the same buffer size for data transmission, and the initial storage space status for Mars relay communications might be influenced by other exploration tasks and diverse in different contact events

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Summary

INTRODUCTION

During the Mars rover exploration phase, it is necessary to send the Mars surface exploration data back to Earth for scientific research and other important applications. In order to further improve the data transmission capacity, several data relay proposals have been studied and developed in past years, such as the Lagrange points L4/L5 of the Sun–Earth system [2], the solar system satellite relay constellation [3], and the Mars orbiter relay communication [4]–[6]. The Consultative Committee for Space Data Systems (CCSDS) has studied and recommended a series of “Proximity-1” protocols with the orbiter-mastered hailing channel and single-access working channel related to the Mars relay communications [8]. In current Earth satellite communications, the most studied access selection schemes [13] include the following. The current methods perform well on the user access to low-Earth satellite constellations

Terms and Definitions
Geometric Model
Constrains and Assumptions
Optimization Function
Algorithm Architecture
Oligopoly Game
Storage Cost
D12 D2
Orbiter Selection
Simulation Situation
Storage Cost Function
CONCLUSION
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