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 |