Navigation in GNSS-Denied Environment Based on Observation of RSOs and Stars

Navigating in an environment, where Global Navigation Satellite System (GNSS) signals are unavailable, presents a formidable challenge. A feasible strategy involves integrating stellar observations with inertial information to realize precise navigation. Inertial/Stellar Celestial Navigation enhances position accuracy by addressing gyro drift through stellar observations. However, the position error still continues to grow over time which arises from unobservable error factors. With improved orbit determination accuracy and the resident space object (RSO) observation method, navigating using RSO observation is gaining viability. This study models the RSO navigation problem as a Perspective-n-Point (PnP) problem and proposes that observing more than 6 RSOs can yield complete solution for position and attitude. Additionally, a tightly coupled navigation algorithm integrating inertial, stellar, and RSO observations is introduced. Simulation validation under dynamic condition demonstrates the algorithm’s efficacy, achieving a position accuracy of 30[Formula: see text]m and an attitude accuracy of 5[Formula: see text]arcsec (RMS) without GNSS data.

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Publication Details

Journal
Guidance Navigation and Control
Published
2024-10-02
DOI
https://doi.org/10.1142/s2737480724500225
Citations
1
Primary Topic
Inertial Sensor and Navigation
Type
article
Field-Weighted Citation Impact
1.30
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Navigation in GNSS-Denied Environment Based on Observation of RSOs and Stars

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article

Navigation in GNSS-Denied Environment Based on Observation of RSOs and Stars

Guoliang Yang, Jiayu Wang, Yu Tian, Yang Weiping, Xiaokun Ding
article en
1 citations

Abstract

Navigating in an environment, where Global Navigation Satellite System (GNSS) signals are unavailable, presents a formidable challenge. A feasible strategy involves integrating stellar observations with inertial information to realize precise navigation. Inertial/Stellar Celestial Navigation enhances position accuracy by addressing gyro drift through stellar observations. However, the position error still continues to grow over time which arises from unobservable error factors. With improved orbit determination accuracy and the resident space object (RSO) observation method, navigating using RSO observation is gaining viability. This study models the RSO navigation problem as a Perspective-n-Point (PnP) problem and proposes that observing more than 6 RSOs can yield complete solution for position and attitude. Additionally, a tightly coupled navigation algorithm integrating inertial, stellar, and RSO observations is introduced. Simulation validation under dynamic condition demonstrates the algorithm’s efficacy, achieving a position accuracy of 30[Formula: see text]m and an attitude accuracy of 5[Formula: see text]arcsec (RMS) without GNSS data.

Guidance Navigation and ControlVol. 05(01)
Northwestern Polytechnical University (CN), Institute of Flight (US)
Life below water
Openalex Percentile: Top 13%
Inertial Sensor and Navigation
1.30
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