Solar sail cooperative formation flying around L2-type artificial equilibrium points W Wang, H Baoyin, G Mengali, AA Quarta Acta Astronautica 169, 224-239, 2020 | 32 | 2020 |
Multiple solar sail formation flying around heliocentric displaced orbit via consensus W Wang, AA Quarta, G Mengali, J Yuan Acta Astronautica 154, 256-267, 2019 | 27 | 2019 |
Decentralized fault-tolerant control for multiple electric sail relative motion at artificial Lagrange points W Wang, G Mengali, AA Quarta, H Baoyin Aerospace Science and Technology 103, 105904, 2020 | 26 | 2020 |
Minimum-time low-thrust many-revolution geocentric trajectories with analytical costates initialization D Wu, W Wang, F Jiang, J Li Aerospace Science and Technology 119, 107146, 2021 | 25 | 2021 |
Distributed adaptive synchronization for multiple spacecraft formation flying around Lagrange point orbits W Wang, G Mengali, AA Quarta, J Yuan Aerospace Science and Technology 74, 93-103, 2018 | 23 | 2018 |
Formation flying for electric sails in displaced orbits. Part II: distributed coordinated control W Wang, G Mengali, AA Quarta, J Yuan Advances in Space Research 60 (6), 1130-1147, 2017 | 19 | 2017 |
Formation flying for electric sails in displaced orbits. Part I: geometrical analysis W Wang, G Mengali, AA Quarta, J Yuan Advances in Space Research 60 (6), 1115-1129, 2017 | 17 | 2017 |
Asteroid Hovering Missions from a Fuel-Consumption Viewpoint W Wang, D Wu, G Mengali, AA Quarta, H Baoyin Journal of Guidance, Control, and Dynamics 43 (7), 1374-1382, 2020 | 16 | 2020 |
Analysis of relative motion in non-Keplerian orbits via modified equinoctial elements W Wang, G Mengali, AA Quarta, J Yuan Aerospace Science and Technology 58, 389-400, 2016 | 15 | 2016 |
Invariant manifold and bounds of relative motion between heliocentric displaced orbits W Wang, J Yuan, G Mengali, AA Quarta Journal of Guidance, Control, and Dynamics 39 (8), 1764-1776, 2016 | 15 | 2016 |
Time-Optimal Formation Establishment Around a Slowly Rotating Asteroid W Wang, G Mengali, AA Quarta, H Baoyin Journal of Guidance, Control, and Dynamics 44 (4), 889-897, 2021 | 12 | 2021 |
Reachable domain of spacecraft with a single normal impulse J Zhang, J Yuan, W Wang, J Wang Aircraft Engineering and Aerospace Technology 91 (7), 977-986, 2019 | 9 | 2019 |
Fuel-optimal spacecraft cluster flight around an ellipsoidal asteroid W Wang, D Wu, H Lei, H Baoyin Journal of Guidance, Control, and Dynamics 44 (10), 1875-1882, 2021 | 8 | 2021 |
Extreme values of relative distances for spacecraft in elliptic displaced orbits W Wang, G Mengali, AA Quarta, J Yuan Advances in Space Research 58 (4), 475-487, 2016 | 7 | 2016 |
Hybrid Sail Displaced Orbits Around Point in the Elliptic Earth-Moon System C Gao, W Wang, J Yuan, L Guo Journal of Guidance, Control, and Dynamics 42 (2), 416-424, 2019 | 5 | 2019 |
Adaptive fault-tolerant control for spacecraft formation under external disturbances with guaranteed performance Y Wu, W Wang, H Zhu, S Wu, CJ Damaren Advances in Space Research 72 (5), 1583-1592, 2023 | 3 | 2023 |
Along-track boundedness condition for spacecraft relative motion around a slowly rotating asteroid W Wang, H Lei, G Mengali, AA Quarta, H Baoyin IEEE Transactions on Aerospace and Electronic Systems, 2023 | 3 | 2023 |
Optimal Projected Circular Orbit for Spacecraft Formation Flying Near a Slowly Rotating Asteroid W Wang, D Wu, R Sun, H Baoyin IEEE Transactions on Aerospace and Electronic Systems 58 (6), 5483-5493, 2022 | 2 | 2022 |
Spacecraft Relative Motion Control Near an Asteroid With Uncertainties: A Lyapunov Redesign Approach W Wang, G Mengali, AA Quarta, H Baoyin IEEE Transactions on Aerospace and Electronic Systems, 2024 | | 2024 |
Distributed Control for Multiple Spacecraft System Near Asteroids with Event-Triggered Strategy R Sun, W Wang, J Wang Journal of Guidance, Control, and Dynamics, 1-10, 2024 | | 2024 |