Abstract

Radio frequency (RF) measurement technology provides a relative navigation solution that can be of great importance to have significant potential for application to the satellite groups. With the development of the RF relative measurement sensors, it is found that the antenna configuration of the sensors affects the precision of relative position and attitude measurement. This study proposes improvements to the precision of the sensors by the virtue of the optimal antenna configuration. Furthermore, the concept of dilution of precision (DOP) is extended to the RF relative measurement sensors, and a new dilution called IDOP is proposed as a benchmark to determine the precision of relative position and attitude measurement in engineering applications of the space mission. In order to select the optimal antenna configuration in real time in a scene where the intersatellite position and attitude change dynamically, this study presents an optimal antenna configuration selection strategy and models the antenna configuration selection as a combinatorial optimization problem. Furthermore, the genetic algorithm (GA) with two encoding mechanisms is proposed to solve this problem. Finally, numerical results are presented to verify the robustness.

Highlights

  • Satellite formation flying (SFF) has brought several advantages and privileges to space missions

  • The onboard embedded systems can be of advantage in a way it enhances the precision achieved by Global Navigation Satellite System (GNSS), and more importantly, it can be used in the deep space where GNSS is not available [5]

  • Formation flying radio frequency (FFRF) sensor is another Radio frequency (RF)-based technology developed by the National Center for Space Studies in the PRISMA mission [9, 10]

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Summary

Introduction

Satellite formation flying (SFF) has brought several advantages and privileges to space missions. In this way, the different requirements of the estimated precision of intersatellite position and attitude parameters in different stages of the space mission can be satisfied. Reference [15] presented this issue in GNSS-based attitude measurement, but the optimal antenna configuration is not obtained, and its model is different from this study. For these reasons, an antenna configuration selection strategy is proposed in this study. The experimental results and conclusion of this paper are shown in Sections 4 and 5, respectively

RF Relative Measurement and DOP Modeling
Antenna Configuration
Antenna Configuration Selection Strategy Based on Genetic Algorithm
Experimental Work and Results
Experiments and Results
Conclusions
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