Year |
Citation |
Score |
2020 |
Gao T, Peng H, Bai X. Calibration of atmospheric density model based on Gaussian Processes Acta Astronautica. 168: 273-281. DOI: 10.1016/J.Actaastro.2019.12.014 |
0.315 |
|
2020 |
Peng H, Bai X. Machine Learning Approach to Improve Satellite Orbit Prediction Accuracy Using Publicly Available Data Journal of the Astronautical Sciences. 67: 762-793. DOI: 10.1007/S40295-019-00158-3 |
0.341 |
|
2019 |
Yang H, Li S, Bai X. Fast Homotopy Method for Asteroid Landing Trajectory Optimization Using Approximate Initial Costates Journal of Guidance Control and Dynamics. 42: 585-597. DOI: 10.2514/1.G003414 |
0.367 |
|
2019 |
Peng H, Bai X. Gaussian Processes for improving orbit prediction accuracy Acta Astronautica. 161: 44-56. DOI: 10.1016/J.Actaastro.2019.05.014 |
0.341 |
|
2018 |
Peng H, Liao Y, Bai X, Xu S. Maintenance of Libration Point Orbit in Elliptic Sun–Mercury Model Ieee Transactions On Aerospace and Electronic Systems. 54: 144-158. DOI: 10.1109/Taes.2017.2739938 |
0.377 |
|
2018 |
Peng H, Bai X. Improving orbit prediction accuracy through supervised machine learning Advances in Space Research. 61: 2628-2646. DOI: 10.1016/J.Asr.2018.03.001 |
0.339 |
|
2018 |
Peng H, Bai X. Natural deep space satellite constellation in the Earth-Moon elliptic system Acta Astronautica. 153: 240-258. DOI: 10.1016/J.Actaastro.2018.01.008 |
0.371 |
|
2018 |
Peng H, Bai X. Recovering area-to-mass ratio of resident space objects through data mining Acta Astronautica. 142: 75-86. DOI: 10.1016/J.Actaastro.2017.09.030 |
0.328 |
|
2018 |
Wang L, Bai X. Quadrotor Autonomous Approaching and Landing on a Vessel Deck Journal of Intelligent and Robotic Systems. 92: 125-143. DOI: 10.1007/S10846-017-0757-5 |
0.31 |
|
2017 |
Peng H, Bai X, Masdemont JJ, Gómez G, Xu S. Libration transfer design using patched elliptic three-body models and graphics processing units Journal of Guidance Control and Dynamics. 40: 3155-3166. DOI: 10.2514/1.G002692 |
0.348 |
|
2017 |
Misra G, Bai X. Task-Constrained Trajectory Planning of Free-Floating Space-Robotic Systems Using Convex Optimization Journal of Guidance Control and Dynamics. 40: 2857-2870. DOI: 10.2514/1.G002405 |
0.308 |
|
2017 |
Yang H, Bai X, Baoyin H. Rapid Generation of Time-Optimal Trajectories for Asteroid Landing via Convex Optimization Journal of Guidance Control and Dynamics. 40: 628-641. DOI: 10.2514/1.G002170 |
0.386 |
|
2017 |
Peng H, Bai X, Xu S. Continuation of periodic orbits in the Sun-Mercury elliptic restricted three-body problem Communications in Nonlinear Science and Numerical Simulation. 47: 1-15. DOI: 10.1016/J.Cnsns.2016.11.005 |
0.311 |
|
2017 |
Yang H, Bai X, Baoyin H. Finite-time control for asteroid hovering and landing via terminal sliding-mode guidance Acta Astronautica. 132: 78-89. DOI: 10.1016/J.Actaastro.2016.12.012 |
0.35 |
|
2017 |
Junkins JL, Younes AB, Woollands RM, Bai X. Efficient and Adaptive Orthogonal Finite Element Representation of the Geopotential The Journal of the Astronautical Sciences. 64: 118-155. DOI: 10.1007/S40295-016-0111-3 |
0.531 |
|
2017 |
Yang H, Baoyin H, Bai X, Li J. Bounded trajectories near collinear-like equilibrium points of elongated asteroids using linear control Astrophysics and Space Science. 362: 27. DOI: 10.1007/S10509-017-3007-1 |
0.319 |
|
2013 |
Junkins JL, Bani Younes A, Woollands RM, Bai X. Picard Iteration, Chebyshev Polynomials and Chebyshev-Picard Methods: Application in Astrodynamics The Journal of the Astronautical Sciences. 60: 623-653. DOI: 10.1007/S40295-015-0061-1 |
0.574 |
|
2012 |
Bai X, Junkins JL. Modified Chebyshev-Picard iteration methods for station-keeping of translunar halo orbits Mathematical Problems in Engineering. 2012. DOI: 10.1155/2012/926158 |
0.57 |
|
2011 |
Bai X, Junkins JL. Modified Chebyshev-Picard iteration methods for solution of boundary value problems Advances in the Astronautical Sciences. 140: 381-400. DOI: 10.1007/S40295-013-0021-6 |
0.558 |
|
2011 |
Bai X, Junkins JL. Modified chebyshev-Picard iteration methods for orbit propagation Journal of the Astronautical Sciences. 58: 583-613. DOI: 10.1007/Bf03321533 |
0.566 |
|
2009 |
Bai X, Junkins JL. New results for time-optimal three-axis reorientation of a rigid spacecraft Journal of Guidance, Control, and Dynamics. 32: 1071-1076. DOI: 10.2514/1.43097 |
0.526 |
|
2009 |
Bai X, Davis JJ, Doebbler J, Turner JD, Junkins JL. Modeling, Control and Simulation of a Novel Mobile Robotic System Engineering Letters. 16: 451-464. DOI: 10.1007/978-1-4020-8919-0_31 |
0.498 |
|
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