| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Academy Transaction note “matrix gains selection for three-axis magnetic attitude control of dynamically elongated satellite”
|
Monakhova, Uliana
|
|
|
224 |
C |
p. 445-448
|
artikel
|
| 2 |
A comprehensive study on PnP-based pipeline for pose estimation of noncooperative satellite
|
Yu, Yingjian
|
|
|
224 |
C |
p. 486-496
|
artikel
|
| 3 |
A computational methodology for invariant manifold connections between quasi-periodic libration point orbits in non-autonomous problems
|
Li, Ruilong
|
|
|
224 |
C |
p. 593-601
|
artikel
|
| 4 |
Aerodynamic coordinated control of attitude and relative position of a formation of microsatellites
|
Sabatini, Marco
|
|
|
224 |
C |
p. 183-194
|
artikel
|
| 5 |
A moderate-Ti lunar mare soil simulant: IGG-01
|
Ruan, Renhao
|
|
|
224 |
C |
p. 148-160
|
artikel
|
| 6 |
An assessment of Dragonfly-Backshell aerodynamics preparing for the initial flight on Titan
|
Zucker, Corey
|
|
|
224 |
C |
p. 127-137
|
artikel
|
| 7 |
An experimental and numerical investigation of ballistic penetration behaviors of deployable composite shells
|
Wu, Chenchen
|
|
|
224 |
C |
p. 533-545
|
artikel
|
| 8 |
Chain tethered satellite formation reconfiguration: An event-triggered practical prescribed-time control approach
|
Li, Qinwen
|
|
|
224 |
C |
p. 436-444
|
artikel
|
| 9 |
Crater identification by perspective cone alignment
|
Chng, Chee-Kheng
|
|
|
224 |
C |
p. 1-16
|
artikel
|
| 10 |
Criteria for selection of point-ahead angle compensation strategy in intersatellite laser ranging interferometry of TianQin based on research of tilt-to-length coupling noise
|
Wang, Jinmeng
|
|
|
224 |
C |
p. 202-214
|
artikel
|
| 11 |
Definitive limitation of orbit prediction error for laser-based debris removal
|
Shibata, Kazunori
|
|
|
224 |
C |
p. 281-290
|
artikel
|
| 12 |
Design and analysis of a novel deployable grasping manipulator for space object capture
|
Xu, Kun
|
|
|
224 |
C |
p. 266-280
|
artikel
|
| 13 |
Design optimization of cubic-shaped pressurant tank for CubeSat propulsion system
|
Shcheglov, Georgy A.
|
|
|
224 |
C |
p. 48-56
|
artikel
|
| 14 |
Development and user study of the Operational Geology in a Virtual Environment (OGIVE) platform
|
Paige, C.
|
|
|
224 |
C |
p. 17-36
|
artikel
|
| 15 |
Development of hybrid landing gear for OMOTENASHI surface probe
|
Otsuki, Masatsugu
|
|
|
224 |
C |
p. 309-324
|
artikel
|
| 16 |
Discrete search-based determination of a local orbital frame in unknown environments
|
Messmann, David
|
|
|
224 |
C |
p. 546-557
|
artikel
|
| 17 |
Editorial Board
|
|
|
|
224 |
C |
p. ii
|
artikel
|
| 18 |
Effect of flameholding cavity geometry on the flowfield of a solid fuel scramjet
|
Prokesch, Youri
|
|
|
224 |
C |
p. 508-519
|
artikel
|
| 19 |
Efficient adversarial attacks detection for deep reinforcement learning-based autonomous planetary landing GNC
|
Wang, Ziwei
|
|
|
224 |
C |
p. 37-47
|
artikel
|
| 20 |
Ejecta velocity and motion model of spherical aluminum alloy projectile hypervelocity impact on basalt
|
Liu, Wenjin
|
|
|
224 |
C |
p. 574-592
|
artikel
|
| 21 |
Endoatmospheric powered descent guidance
|
Wang, Jiawei
|
|
|
224 |
C |
p. 112-121
|
artikel
|
| 22 |
Experimental study and performance analysis of a dual-mode space propulsion system pressurized by electric pump
|
Li, Tianwen
|
|
|
224 |
C |
p. 497-507
|
artikel
|
| 23 |
Extended perilune rendezvous method for low Delta-V transition to NRHO for cargo transportation mission to gateway
|
Kikuchi, Junji
|
|
|
224 |
C |
p. 89-98
|
artikel
|
| 24 |
IAA-PDC-23-09-20 low-cost mission architectures to small bodies
|
Freeman, Anthony
|
|
|
224 |
C |
p. 122-126
|
artikel
|
| 25 |
Ignition and flow combustion characteristics of hydroxylammonium nitrate - based liquid propellant based on electric method
|
Jin, Bao-zhi
|
|
|
224 |
C |
p. 172-182
|
artikel
|
| 26 |
Impact of energy deposition as active flow control on scramjet inlet performance using Immersed Boundary Method
|
Pathak, Amrita
|
|
|
224 |
C |
p. 291-308
|
artikel
|
| 27 |
Investigation on the effect of the leading angle of the strut on the stabilization characteristics of lifted jet flames
|
Zhao, Zi-jian
|
|
|
224 |
C |
p. 520-532
|
artikel
|
| 28 |
Lifetime experiment and analysis of an electrowetting ionic liquid electrospray thruster
|
Sun, Wei
|
|
|
224 |
C |
p. 465-470
|
artikel
|
| 29 |
Liquid propellant rocket engine cycles partially using electric turbopump
|
Shoyama, Tadayoshi
|
|
|
224 |
C |
p. 138-147
|
artikel
|
| 30 |
Magnetic field dynamics and noise analysis for space-based GW detector in far-earth orbits: A hybrid modeling approach
|
Low, Kian Hong
|
|
|
224 |
C |
p. 99-111
|
artikel
|
| 31 |
Mainardi smoothing homotopy method for solving nonlinear optimal control problems
|
Qing, Wenjie
|
|
|
224 |
C |
p. 471-485
|
artikel
|
| 32 |
Mission design for space telescope servicing at Sun–Earth L2
|
Pascarella, Alex
|
|
|
224 |
C |
p. 397-414
|
artikel
|
| 33 |
Modeling of microgravity conditions on earth in the study of multiphase flows
|
Skryleva, E.I.
|
|
|
224 |
C |
p. 449-457
|
artikel
|
| 34 |
Multidisciplinary design analysis and optimization of the aerodynamic shape of the SpaceLiner passenger stage
|
Mauriello, Tommaso
|
|
|
224 |
C |
p. 244-265
|
artikel
|
| 35 |
Nonlinear modeling and validation of spacecraft dynamics for space-based gravitational wave detector
|
Zhang, Dexuan
|
|
|
224 |
C |
p. 57-68
|
artikel
|
| 36 |
On metallic-type asteroid rotation moving in magnetic field (introducing magnetic second-grade YORP effect)
|
Ershkov, S.V.
|
|
|
224 |
C |
p. 195-201
|
artikel
|
| 37 |
Orbit determination for spacecraft with continuous low-thrust using nonsingular Thrust-Fourier-Coefficients and filtering-through approach
|
Zhang, JiDan
|
|
|
224 |
C |
p. 353-366
|
artikel
|
| 38 |
Oxygen production by solar vapor-phase pyrolysis of lunar regolith simulant
|
Šeško, Rok
|
|
|
224 |
C |
p. 215-225
|
artikel
|
| 39 |
Path planning of 6-DOF free-floating space robotic manipulators using reinforcement learning
|
Al Ali, Ahmad
|
|
|
224 |
C |
p. 367-378
|
artikel
|
| 40 |
Performance evaluation of a low power Hall thruster with carbon dioxide propellant
|
Tsuchikawa, Seiya
|
|
|
224 |
C |
p. 415-426
|
artikel
|
| 41 |
Qualitative analysis of the presence of gaze-evoked nystagmus in astronauts after long term space flights. Results of “field test” experiment
|
Tomilovskaya, Elena
|
|
|
224 |
C |
p. 82-88
|
artikel
|
| 42 |
Quantifying the risk of medical evacuation in spaceflight
|
Anderson, Arian
|
|
|
224 |
C |
p. 458-464
|
artikel
|
| 43 |
Real-time fault-tolerant guidance for launch vehicle ascending flight under thrust drop failure
|
Ma, Zhenwei
|
|
|
224 |
C |
p. 338-352
|
artikel
|
| 44 |
Reinforcement learning-based multi-impulse rendezvous approach for satellite constellation reconfiguration
|
Xu, Longwei
|
|
|
224 |
C |
p. 325-337
|
artikel
|
| 45 |
Research on the flame oscillation characteristics of scramjet combustor equipped with strut fuel injector
|
Quan, Fuxu
|
|
|
224 |
C |
p. 558-573
|
artikel
|
| 46 |
Safety of using hydrogen: Suppression of detonation in hydrogen-air mixtures
|
Smirnov, N.N.
|
|
|
224 |
C |
p. 69-81
|
artikel
|
| 47 |
Simulating lunar highlands regolith profiles on Earth to inform infrastructure development and ISRU activities on the Moon
|
Lucas, Michael P.
|
|
|
224 |
C |
p. 161-171
|
artikel
|
| 48 |
The effect of projectile nose shape on the formation and expansion of impact-induced ejecta for sand target
|
Zhang, Hongyu
|
|
|
224 |
C |
p. 427-435
|
artikel
|
| 49 |
Towards robotic on-orbit assembly of large space telescopes: Mission architectures, concepts, and analyses
|
Nanjangud, Angadh
|
|
|
224 |
C |
p. 379-396
|
artikel
|
| 50 |
Vibration-attitude integrated control of large membrane diffraction space telescope
|
Yu, Heng
|
|
|
224 |
C |
p. 602-621
|
artikel
|
| 51 |
Wireless power transfer in space using flexible, lightweight, coherent arrays
|
Ayling, Alex
|
|
|
224 |
C |
p. 226-243
|
artikel
|
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