| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Adaptive generalized ZEM-ZEV feedback guidance for planetary landing via a deep reinforcement learning approach
|
Furfaro, Roberto
|
|
|
171 |
C |
p. 156-171
|
artikel
|
| 2 |
Aerothermodynamics modelling of complex shapes in the DEBRISK atmospheric reentry tool: Methodology and validation
|
Annaloro, Julien
|
|
|
171 |
C |
p. 388-402
|
artikel
|
| 3 |
Analytical cooperative entry guidance for Rendezvous and formation flight
|
Yu, Wenbin
|
|
|
171 |
C |
p. 118-138
|
artikel
|
| 4 |
A new variant of the B-dot control for spacecraft magnetic detumbling
|
Desouky, Mohammed A.A.
|
|
|
171 |
C |
p. 14-22
|
artikel
|
| 5 |
Centralized visual based navigation and control of a swarm of satellites for on-orbit servicing
|
Sabatini, M.
|
|
|
171 |
C |
p. 323-334
|
artikel
|
| 6 |
Challenge-Based Learning in Aerospace Engineering Education: The ESA Concurrent Engineering Challenge at the Technical University of Madrid
|
López-Fernández, D.
|
|
|
171 |
C |
p. 369-377
|
artikel
|
| 7 |
Command-centric architecture (C2A): Satellite software architecture with a flexible reconfiguration capability
|
Nakajima, Shintaro
|
|
|
171 |
C |
p. 208-214
|
artikel
|
| 8 |
Deep space transportation enhanced by 20 kW-Class Hall Thrusters
|
Paissoni, C.A.
|
|
|
171 |
C |
p. 83-96
|
artikel
|
| 9 |
Diffusion phenomenon of lunar soil particles under a plume in a vacuum environment by numerical simulation
|
Bo, Zhigang
|
|
|
171 |
C |
p. 403-414
|
artikel
|
| 10 |
Dynamic characteristics of a gliding arc plasma-assisted ignition in a cavity-based scramjet combustor
|
Feng, Rong
|
|
|
171 |
C |
p. 238-244
|
artikel
|
| 11 |
Effect of coaxial injector parameters on LOX/methane engines: A numerical analysis
|
Xu, Jiabao
|
|
|
171 |
C |
p. 225-237
|
artikel
|
| 12 |
Experimental investigation on automated assembly of space structure from cooperative modular components
|
Lu, Yun
|
|
|
171 |
C |
p. 378-387
|
artikel
|
| 13 |
Experimental investigation on the effect of ionization seed mass fraction on gas plasma jet deflection
|
Zhao, Kai
|
|
|
171 |
C |
p. 257-264
|
artikel
|
| 14 |
Experimental research on the shock wave control based on one power supply driven plasma synthetic jet actuator array
|
Zhang, Zhibo
|
|
|
171 |
C |
p. 359-368
|
artikel
|
| 15 |
Hardware-in-the-loop testing of formation flying control and sensing algorithms for starshade missions
|
Palacios, Leonel M.
|
|
|
171 |
C |
p. 97-105
|
artikel
|
| 16 |
Hayabusa2 mission status: Landing, roving and cratering on asteroid Ryugu
|
Tsuda, Yuichi
|
|
|
171 |
C |
p. 42-54
|
artikel
|
| 17 |
Hypersonic drag reduction mechanism of a novel combinational spike and multi-opposing jets aerodynamic configuration
|
Huang, Jie
|
|
|
171 |
C |
p. 245-256
|
artikel
|
| 18 |
IFC - Publication Information
|
|
|
|
171 |
C |
p. IFC
|
artikel
|
| 19 |
Investigation of pyrolysis effect on convective heat transfer characteristics of supercritical aviation kerosene
|
Jiao, Si
|
|
|
171 |
C |
p. 55-68
|
artikel
|
| 20 |
Modeling the micro-explosion of miscible and immiscible liquid droplets
|
Antonov, D.V.
|
|
|
171 |
C |
p. 69-82
|
artikel
|
| 21 |
New fly-around formations for an elliptical reference orbit
|
Bai, Shengzhou
|
|
|
171 |
C |
p. 335-351
|
artikel
|
| 22 |
Novel formula for pyrolysis rate of charring materials under different heating rates
|
Guo, Jin
|
|
|
171 |
C |
p. 352-358
|
artikel
|
| 23 |
Numerical simulation of the hypervelocity impact of the ball and the spherical containment in three-material statement
|
Smirnov, N.N.
|
|
|
171 |
C |
p. 215-224
|
artikel
|
| 24 |
Optimal rendezvous trajectory between Sample Return Orbiter and Orbiting Sample Container in a Mars Sample Return mission
|
Fossà, Alberto
|
|
|
171 |
C |
p. 31-41
|
artikel
|
| 25 |
Orbital boost characteristics of spacecraft by electrodynamic tethers with consideration of electric-magnetic-dynamic energy coupling
|
Liu, Jinyu
|
|
|
171 |
C |
p. 196-207
|
artikel
|
| 26 |
Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows
|
Ju, Shengjun
|
|
|
171 |
C |
p. 300-310
|
artikel
|
| 27 |
Path planning for asteroid hopping rovers with pre-trained deep reinforcement learning architectures
|
Jiang, Jianxun
|
|
|
171 |
C |
p. 265-279
|
artikel
|
| 28 |
Performance optimization of a krypton Hall thruster with a rotating propellant supply
|
Xia, Guojun
|
|
|
171 |
C |
p. 290-299
|
artikel
|
| 29 |
Radiation engineering analysis of shielding materials to assess their ability to protect astronauts in deep space from energetic particle radiation
|
Manning, Bryan
|
|
|
171 |
C |
p. 23-30
|
artikel
|
| 30 |
Rapid trajectory design in complex environments enabled by reinforcement learning and graph search strategies
|
Das-Stuart, A.
|
|
|
171 |
C |
p. 172-195
|
artikel
|
| 31 |
Spacecraft trajectory tracking and parameter estimation around a splitting contact binary asteroid
|
Silva, Tiago M.
|
|
|
171 |
C |
p. 280-289
|
artikel
|
| 32 |
System scheme design for LOX/LCH4 variable thrust liquid rocket engines using motor pump
|
Cui, Peng
|
|
|
171 |
C |
p. 139-150
|
artikel
|
| 33 |
Terminal adaptive guidance via reinforcement meta-learning: Applications to autonomous asteroid close-proximity operations
|
Gaudet, Brian
|
|
|
171 |
C |
p. 1-13
|
artikel
|
| 34 |
Thermal shelter for survival of rover during cryogenic lunar night
|
Kim, Taig Young
|
|
|
171 |
C |
p. 151-155
|
artikel
|
| 35 |
Trajectory optimization for rendezvous with bearing-only tracking
|
Chu, Xiaoyu
|
|
|
171 |
C |
p. 311-322
|
artikel
|
| 36 |
Vertex combination approach for uncertainty propagation analysis in spacecraft structural system with complex eigenvalue
|
Qiu, Zhiping
|
|
|
171 |
C |
p. 106-117
|
artikel
|
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