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
39 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
33 2021 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
30 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
28 2020 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
27 2018 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
24 2020 Nonlinear guidance laws for maneuvering target interception with virtual look angle constraint Y Wang, H Wang, D Lin, W Wang
IEEE Transactions on Aerospace and Electronic Systems 58 (4), 2807-2822, 2021
19 2021 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 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
17 2021 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 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
17 2016 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
15 2021 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
14 2016 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
12 2024 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
11 2023 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
11 2019 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
8 2022 Hybrid Sail Displaced Orbits Around C Gao, W Wang, J Yuan, L Guo
Journal of Guidance, Control, and Dynamics 42 (2), 416-424, 2019
7 2019 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 Distributed control for multiple spacecraft system near asteroids with event-triggered strategy R Sun, W Wang, J Wang
Journal of Guidance, Control, and Dynamics 47 (5), 1005-1014, 2024
6 2024 
Alessandro QuartapisaEmail được xác minh tại ing.unipi.it
