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    Chapter and Conference Paper

    Intelligent Fault Diagnosis Method of Inertial Sensors for Space Gravitational Wave Detection

    Space inertial sensor is one of the key loads in space gravitational wave detection mission. Once it fails, the entire mission is likely to be affected or even fail. The existing data-driven intelligent fault ...

    Cheng Bi, **aokui Yue, Yibo Ding in Computational and Experimental Simulations… (2024)

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    Chapter and Conference Paper

    Fuzzy-Logic-Based Integrated Orbit-Attitude-Vibration Prescribed-Time Control for Large-Scale Flexible Spacecraft

    This paper investigates a fuzzy-logic-based integrated orbit-attitude-vibration prescribed-time controller for large-scale flexible spacecraft to achieve the high-precision orbit-attitude-vibration stabilizati...

    **aokui Yue, Bailiang Lyu, Chuang Liu in Computational and Experimental Simulations… (2024)

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    Chapter and Conference Paper

    An Intelligent Penetration Guidance Law Based on DDPG for Hypersonic Vehicle

    A novel intelligent guidance law based on Deep Deterministic Policy Gradient (DDPG) is devised in this paper to deal with problems of penetration for hypersonic boost glide vehicle (HBGV). Firstly, an agent ba...

    Rongyi Guo, Yibo Ding, **aokui Yue in Computational and Experimental Simulations… (2024)

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    Chapter and Conference Paper

    Deep Reinforcement Learning-Based Intelligent Decision-Making for Orbital Game of Satellite Swarm

    Recent years have witnessed the rapid development of aerospace science and technology, and the orbital game technology has shown great potential value in the field of failed satellite maintenance, debris remov...

    Weizhuo Yu, **aokui Yue, Panxing Huang in Computational and Experimental Simulations… (2024)

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    Chapter and Conference Paper

    Neural Adaptive Finite-Time Sliding Mode Controller for Air-Breathing Hypersonic Vehicle

    A neural adaptive sliding mode controller (NASMC) composed of an adaptive finite-time sliding mode controller (AFSMC) with the long short-term memory (LSTM)-based deep recurrent neural network is presented for...

    Tianchen Zhang, Yibo Ding, **aokui Yue in Computational and Experimental Simulations… (2024)

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    Chapter and Conference Paper

    Robust H Attitude Stabilization for the Cluster Takeover of Non-cooperative Flexible Spacecraft

    In this paper, a cooperative control scheme based on the small spacecraft cluster is proposed for the takeover control of the failed flexible spacecraft in space. In order to overcome external disturbance, ine...

    **aokui Yue, Ziyu Yang, Hongyu Yu in Computational and Experimental Simulations… (2024)

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    Chapter and Conference Paper

    Connectivity Preservation and Collision Avoidance Control for Spacecraft Formation Flying with Bounded Actuation

    This paper considers connectivity preservation and collision avoidance controller design for spacecraft formation flying with bounded actuation. A distributed controller with bounded artificial potential funct...

    **anghong Xue, **aokui Yue, Jian** Yuan in Advances in Guidance, Navigation and Control (2022)

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    Chapter and Conference Paper

    Research on Decision Method of Spacecraft Cluster Combination Mode for In-Orbit Service

    In order to meet the requirements of in-orbit service, the spacecraft cluster is designed to expand and maintain the functions of cooperative in-orbit spacecraft. In order to improve the autonomy of spacecraft...

    Bosong Wei, **aokui Yue in Advances in Guidance, Navigation and Control (2022)

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    Chapter and Conference Paper

    Orbit Determination Using Combined GPS + Beidou Observations for Low Earth Cubesats: Software Validation in Ground Testbed

    Nowadays, satellites in low earth orbit (LEO) can benefit from Global Navigation Satellite System (GNSS), such as Global Positioning System (GPS) of United States, to estimate positions and velocities. As Chin...

    Yang Yang, **aokui Yue, Geshi Tang in China Satellite Navigation Conference (CSN… (2015)

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    Chapter and Conference Paper

    GPS Receiver Clock Modelling for Kinematic-Based Precise Orbit Determination of Low Earth Orbiters

    This paper describes a GPS receiver clock model that can improve the accuracy of kinematic orbit determination for spacecraft in low earth orbit. The receiver clock error is commonly estimated on an epoch-by-e...

    Yang Yang, **aokui Yue, Yong Li, Chris Rizos in China Satellite Navigation Conference (CSN… (2014)