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Attitude control in spacecraft orbit-raising using a reduced quaternion model JOURNAL ARTICLE published 25 October 2014 in Advances in aircraft and spacecraft science |
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Self-triggered formation attitude control for multiple spacecraft with disturbances JOURNAL ARTICLE published May 2024 in Advances in Space Research |
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Momentum Space Analysis for Mixed Skew Angle Arrays BOOK CHAPTER published 15 January 2020 in Advances in Spacecraft Attitude Control |
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Investigations of an integrated angular velocity measurement and attitude control system for spacecraft using magnetically suspended double-gimbal CMGs JOURNAL ARTICLE published June 2013 in Advances in Space Research |
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Attitude control for on-orbit servicing spacecraft using hybrid actuator JOURNAL ARTICLE published March 2018 in Advances in Space Research Research funded by National Key Research and Development Plan (2016YFB0500901) | Open Fund of National Defense Key Discipline Laboratory of Micro-Spacecraft Technology (HIT.KLOF.MST.201705) | Fundamental Research Funds for the Central Universities (NZ2016111) |
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Spacecraft quaternion based attitude input-output feedback linearization control using reaction wheels PROCEEDINGS ARTICLE published June 2017 in 2017 8th International Conference on Recent Advances in Space Technologies (RAST) |
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Tracking Control of Spacecraft by Dynamic Output Feedback - Passivity-Based Approach BOOK CHAPTER published 14 February 2011 in Advances in Spacecraft Technologies |
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Multi-spacecraft attitude cooperative control using model-based event-triggered methodology JOURNAL ARTICLE published November 2018 in Advances in Space Research Research funded by National Natural Science Foundation of China (11502142,61703276) |
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Robust attitude consensus control for multiple spacecraft systems with unknown disturbances via variable structure control and adaptive sliding mode control JOURNAL ARTICLE published February 2022 in Advances in Space Research Research funded by National Natural Science Foundation of China (61690210,61690213) |
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Investigation of Singularities in a 3/4 CMG Configuration with Mixed Skew Angles BOOK CHAPTER published 15 January 2020 in Advances in Spacecraft Attitude Control |
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Mixed Skew Angle Singularity Plotting for Non-Redundant Single Gimbal CMG Array BOOK CHAPTER published 15 January 2020 in Advances in Spacecraft Attitude Control |
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Generalized predictive tracking control of spacecraft attitude based on hyperbolic tangent extended state observer JOURNAL ARTICLE published July 2020 in Advances in Space Research Research funded by National Natural Science Foundation of China (61903025) | China Scholarship Council (201906465028) | Fundamental Research Funds for the Central Universities (FRF-GF-18-028B) |
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Convergence guaranteed attitude control of underactuated spacecraft using two control torques JOURNAL ARTICLE published March 2024 in Advances in Space Research Research funded by National Natural Science Foundation of China (12302043,62273033) |
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Single Axis Singularity Mapping for Mixed Skew Angle, Non-Redundant, Single Gimbaled CMG Systems BOOK CHAPTER published 15 January 2020 in Advances in Spacecraft Attitude Control |
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An NDO-Based Adaptive Slide Mode Control Method with Prescribed Settling Time and Its Application in the Integrated Orbit & Attitude Control of Spacecraft BOOK CHAPTER published 2022 in Lecture Notes in Electrical Engineering |
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Feedback attitude control of spacecraft using two single gimbal control moment gyros JOURNAL ARTICLE published October 2021 in Advances in Space Research Research funded by Japan Society for the Promotion of Science (JP19K04837) |
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A Chattering Mitigating Sliding Mode Control for Rigid Spacecraft Attitude Control Maneuver PROCEEDINGS ARTICLE published 21 August 2020 in 2020 International Conference on Advances in Computing, Communication & Materials (ICACCM) |
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Differential Game-Based Interceptor Missile Guidance BOOK CHAPTER published 19 April 2016 in Advances in Missile Guidance, Control, and Estimation |
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Shape-based approach to attitude motion planning of reconfigurable spacecraft JOURNAL ARTICLE published September 2022 in Advances in Space Research Research funded by National Natural Science Foundation of China (11772167,11822205) |
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Finite-Time Control for Combination Spacecraft Attitude Based on LESO of Auxiliary System BOOK CHAPTER published 2023 in Lecture Notes in Electrical Engineering |