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                             29 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 A dimension-reduction solution of free-time differential games for spacecraft pursuit-evasion Li, Zhen-yu
2019
163 PB p. 201-210
artikel
2 A hybrid method based on invariant manifold and chaos control for earth-moon low-energy transfer Zheng, Yue
2019
163 PB p. 145-156
artikel
3 A new gyroscopic principle. New gyroscopic effects on cold atoms and on de Broglie waves, different from the Sagnac effect Krobka, Nikolay I.
2019
163 PB p. 181-189
artikel
4 A new multi-satellite autonomous mission allocation and planning method Du, Bin
2019
163 PB p. 287-298
artikel
5 Attitude motion path planning on Lyapunov periodic orbits in the circular restricted three-body problem Yu, Mo-yao
2019
163 PB p. 168-180
artikel
6 Augmented unbiased minimum-variance input and state estimation for tracking a maneuvering satellite Jiang, Yuzi
2019
163 PB p. 96-107
artikel
7 Concurrent co-location maneuver planning for geostationary satellites Satpute, Sumeet
2019
163 PB p. 211-224
artikel
8 Decomposition analysis of spacecraft relative motion with different inter-satellite ranges Chao, Jiang
2019
163 PB p. 56-68
artikel
9 Editorial Luo, Ya-Zhong
2019
163 PB p. 1-2
artikel
10 Finite time sliding sector control for spacecraft atmospheric entry guidance Xu, Biao
2019
163 PB p. 108-113
artikel
11 Geostationary station-keeping with electric propulsion in full and failure modes Li, Lincheng
2019
163 PB p. 130-144
artikel
12 Global search for periodic orbits in the irregular gravity field of a binary asteroid system Shi, Yu
2019
163 PB p. 11-23
artikel
13 Halo orbits construction based on invariant manifold technique Qian, Ying-Jing
2019
163 PB p. 24-37
artikel
14 High-order state transition polynomial with time expansion based on differential algebra Sun, Zhen-Jiang
2019
163 PB p. 45-55
artikel
15 IFC - Publication Information 2019
163 PB p. IFC
artikel
16 Integrated guidance for Mars entry and powered descent using reinforcement learning and pseudospectral method Jiang, Xiuqiang
2019
163 PB p. 114-129
artikel
17 Integrated orbit determination and maintenance in Earth-Moon unstable dynamics environment Zhou, Yang
2019
163 PB p. 69-76
artikel
18 Maneuver-free approach to range-only initial relative orbit determination for spacecraft proximity operations Gong, Baichun
2019
163 PB p. 87-95
artikel
19 Mars entry trajectory robust optimization based on evidence under epistemic uncertainty Huang, Yuechen
2019
163 PB p. 225-237
artikel
20 Observability analysis and autonomous navigation for two satellites with relative position measurements Li, Yong
2019
163 PB p. 77-86
artikel
21 Optimal commands based multi-stage drag de-orbit design for a tethered system during large space debris removal Chu, Zhongyi
2019
163 PB p. 238-249
artikel
22 Optimal scheduling for location geosynchronous satellites refueling problem Zhang, Tian-Jiao
2019
163 PB p. 264-271
artikel
23 Optimization of aeroassisted rendezvous and interception trajectories between non-coplanar elliptical orbits Han, Hongwei
2019
163 PB p. 190-200
artikel
24 Planetary landing site detection and selection using multilevel optimization strategy Liu, Xu
2019
163 PB p. 272-286
artikel
25 Station-keeping of libration point orbits by means of projecting to the manifolds Zhang, Hanqing
2019
163 PB p. 38-44
artikel
26 The motion of surface particles for the asteroid 101955 Bennu Zhang, Yonglong
2019
163 PB p. 3-10
artikel
27 The satellite layout optimization design approach for minimizing the residual magnetic flux density of micro- and nano-satellites Chen, Xianqi
2019
163 PB p. 299-306
artikel
28 Time-varying state-space model identification of an on-orbit rigid-flexible coupling spacecraft using an improved predictor-based recursive subspace algorithm Ni, Zhiyu
2019
163 PB p. 157-167
artikel
29 Visibility optimization of satellite constellations using a hybrid method Han, Chao
2019
163 PB p. 250-263
artikel
                             29 gevonden resultaten
 
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