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Navigation performance analysis of Earth–Moon spacecraft using GNSS, INS, and star tracker
Global Navigation Satellite System (GNSS) can provide an approach for spacecraft autonomous navigation in earth–moon space to make up for the...
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Feasibility analysis of angles-only navigation algorithm with multisensor data fusion for spacecraft noncooperative rendezvous
Relative navigation is crucial for spacecraft noncooperative rendezvous, and angles-only navigation using visible and infrared cameras provides a...
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Review of Angles-Only Navigation Technique for Spacecraft Autonomous Rendezvous and Docking
Since the navigation sensors used in angles-only navigation are simple, angles-only navigation will be a critical enabling technique for spacecraft...
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Artificial intelligence for spacecraft guidance, navigation, and control: a state-of-the-art
This article reviews state-of-the-art of the problem of using Artificial Intelligence (AI) for spacecraft Guidance, Navigation, and Control (GNC)....
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Spacecraft Celestial Navigation Method Based on Laser Ranging Auxiliary
The method of pure angle observation has serious nonlinearity in celestial navigation system, the angle measurement error is converted to a large...
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Autonomous Guidance, Navigation, and Control of Spacecraft
The autonomous guidance, navigation, and control (GNC) system is an essential component of a spacecraft. It serves the purposes of determining the...
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Reliability Engineering of BeiDou Navigation Satellite
This book describes the reliability research results and experience of BeiDou navigation satellite in engineering development. According to the...
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Software-in-the-Loop Validation of a Novel Two-Point Optimal Guidance for Perturbed Spacecraft Rendezvous and Formations
A novel guidance law that utilizes optimal control theory in combination with linear time-varying state-transition matrices to calculate the optimal...
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A Multi-source Data Fusion Navigation Method of Spacecraft with Limited GNSS Signals
Global Navigation Satellite system (GNSS) is initially designed to provide services to objects on the earth surfaces, or in the earth-orbits with...
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Analysis, Design, and Optimization of Robust Trajectories in Cislunar Environment for Limited-Capability Spacecraft
Nowadays, the space exploration is going in the direction of exploiting small platforms to get high scientific return at significantly lower costs....
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Spacecraft System
The system concept of spacecraft is explained in the chapter, and to whether it is manned or not, the classification of spacecraft is systematically...
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Optical Flow as a Virtual Gyro and Altimeter for Safer Spacecraft Visual Inertial Target Approaches
A high burden lies on the autonomous onboard guidance and navigation system of spacecraft to reliably perform a given maneuver even if parts of the...
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Spacecraft Formation Kee** and Reconfiguration Using Optimal Visual Servoing
This paper proposes a direct visual servoing system for spacecraft guidance in formation flying scenarios. The proposed image-based visual servoing...
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Deep Learning-Based Inertial Navigation Technology for Autonomous Underwater Vehicle Long-Distance Navigation—A Review
AbstractAutonomous navigation technology is the key technology for Autonomous Underwater Vehicle (AUV) to achieve automated, intelligent operation...
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RELATIVE NAVIGATION USING ARTIFICIAL MAGNETIC FIELDS
We show that magnetometer sensing of artificially generated magnetic fields may be used for relative navigation. Two artificial field emitters are...
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Study of the Possibility to Develop a Lunar Navigation Satellite System and a Lunar Orbital Spaceport Using the High Circular Orbits of the Moon Artificial Satellite
AbstractThe paper discusses the development of a lunar navigation satellite system and a lunar orbital spaceport based on high near-circular orbits...
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Observer-based Attitude Maneuver Control of Flexible Spacecraft: A Parametric Approach
To address the problem of control performance degradation caused by flexible attachment vibrations and external disturbances during attitude...
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Decomposed Algorithm for Spacecraft Attitude Estimation in Stellar Correction Mode
AbstractThe paper discusses the problem of a spacecraft attitude estimation and its solution by integrating the measurement data from an...
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OSIRIS-REX POST-TAG OBSERVATION TRAJECTORY DESIGN AND NAVIGATION PERFORMANCE
NASA’s OSIRIS-REx spacecraft successfully collected a sample of asteroid regolith from the surface of near-Earth asteroid Bennu in October of 2020....
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Research on GNSS Navigation Method of Lunar Orbiting Spacecraft Based on Ground Enhancement
With the continuous development of the lunar exploration mission, it is very important to obtain the real-time and accurate position, speed, and time...