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Wei Wang
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Year
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
322020
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
272019
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
262020
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
252021
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
232018
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
192017
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
172017
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
162020
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
152016
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
152016
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
122021
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
92019
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
82021
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
72016
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
52019
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
32023
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
32023
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
22022
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
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Articles 1–20