| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active vibration control of underactuated free-floating spacecraft via a performance enhanced way
|
Wei, Caisheng
|
|
2019
|
157 |
C |
p. 477-488
|
artikel
|
| 2 |
A linear model for relative motion in an elliptical orbit based on a spherical coordinate system
|
Han, Chao
|
|
2019
|
157 |
C |
p. 465-476
|
artikel
|
| 3 |
A location-routing problem for the design of an asteroid mining supply chain network
|
Dorrington, S.
|
|
2019
|
157 |
C |
p. 350-373
|
artikel
|
| 4 |
A new nonlinear Type3-PLL with noise rejection and fast locking performance in tracking telemetry and command systems
|
Zhu, Congying
|
|
2019
|
157 |
C |
p. 397-403
|
artikel
|
| 5 |
An international and interdisciplinary approach on learning how to design a space station
|
Detrell, Gisela
|
|
2019
|
157 |
C |
p. 489-499
|
artikel
|
| 6 |
Approximation for attraction field of irregular celestial bodies using four massive points
|
Burov, Alexander A.
|
|
2019
|
157 |
C |
p. 225-232
|
artikel
|
| 7 |
A space surveillance satellite for cataloging high-altitude small debris
|
Du, Jianli
|
|
2019
|
157 |
C |
p. 268-275
|
artikel
|
| 8 |
A study of droplets emission in Ultrasonic Electric Propulsion system: Experiment and simulation
|
Kang, Xiaoming
|
|
2019
|
157 |
C |
p. 321-331
|
artikel
|
| 9 |
Automated near real-time validation and exploitation of optical sensor data for improved orbital safety
|
Kelecy, Thomas
|
|
2019
|
157 |
C |
p. 404-414
|
artikel
|
| 10 |
Bounded lunar relative orbits
|
Nie, Tao
|
|
2019
|
157 |
C |
p. 500-516
|
artikel
|
| 11 |
Cavity enhanced jet interactions in a scramjet combustor
|
Roos, Tim
|
|
2019
|
157 |
C |
p. 162-179
|
artikel
|
| 12 |
Cosmopolitical bodies: An architecture of space
|
Patrick, Mikaela
|
|
2019
|
157 |
C |
p. 215-224
|
artikel
|
| 13 |
Deployment control of tethered space systems with explicit velocity constraint and invariance principle
|
Murugathasan, Latheepan
|
|
2019
|
157 |
C |
p. 390-396
|
artikel
|
| 14 |
Design and performance evaluation of a piezoelectric aeroelastic energy harvester based on the limit cycle oscillation phenomenon
|
Elahi, Hassan
|
|
2019
|
157 |
C |
p. 233-240
|
artikel
|
| 15 |
Design-build-launch: a hybrid project-based laboratory course for aerospace engineering education
|
Spearrin, R. Mitchell
|
|
2019
|
157 |
C |
p. 29-39
|
artikel
|
| 16 |
Do astronauts benefit from autonomy? Investigating perceived autonomy-supportive communication by Mission Support, crew motivation and collaboration during HI-SEAS 1
|
Goemaere, Sophie
|
|
2019
|
157 |
C |
p. 9-16
|
artikel
|
| 17 |
Efficient gravity field modeling method for small bodies based on Gaussian process regression
|
Gao, Ai
|
|
2019
|
157 |
C |
p. 73-91
|
artikel
|
| 18 |
Energy-optimal spacecraft attitude maneuver path-planning under complex constraints
|
Wu, Changqing
|
|
2019
|
157 |
C |
p. 415-424
|
artikel
|
| 19 |
Evacuation method and outgassing rate of a lunar regolith simulant for deep drilling tests
|
Zhang, Tao
|
|
2019
|
157 |
C |
p. 455-464
|
artikel
|
| 20 |
Experimental investigation on propagation characteristics of rotating detonation wave with a hydrogen-ethylene-acetylene fuel
|
Zhou, Shengbing
|
|
2019
|
157 |
C |
p. 310-320
|
artikel
|
| 21 |
Experimental study of flame stabilization in a kerosene fueled scramjet combustor
|
Wang, Yu-hang
|
|
2019
|
157 |
C |
p. 282-293
|
artikel
|
| 22 |
Experimental study on erosion characteristics of char layer of EPDM composite by cold flow
|
Li, Jiang
|
|
2019
|
157 |
C |
p. 332-340
|
artikel
|
| 23 |
Extension of stable terminator orbits around small bodies
|
Oki, Yusuke
|
|
2019
|
157 |
C |
p. 180-188
|
artikel
|
| 24 |
Fixed-time velocity reconstruction scheme for space teleoperation systems: Exp Barrier Lyapunov Function approach
|
Wang, Ziwei
|
|
2019
|
157 |
C |
p. 92-101
|
artikel
|
| 25 |
Gas-particle two-way coupled method for simulating the interaction between a rocket plume and lunar dust
|
Li, Yang
|
|
2019
|
157 |
C |
p. 123-133
|
artikel
|
| 26 |
Geometry shape selection of NACA airfoils for Mars rotorcraft
|
Zhao, Pengyue
|
|
2019
|
157 |
C |
p. 300-309
|
artikel
|
| 27 |
Globally asymptotic three-axis attitude control for a two-wheeled small satellite
|
Ousaloo, Hamed Shahmohamadi
|
|
2019
|
157 |
C |
p. 17-28
|
artikel
|
| 28 |
IFC - Publication Information
|
|
|
2019
|
157 |
C |
p. IFC
|
artikel
|
| 29 |
Investigation of turbulence flow characteristics in a dual-mode scramjet combustor using hydroxyl tagging velocimetry
|
Ye, Jingfeng
|
|
2019
|
157 |
C |
p. 276-281
|
artikel
|
| 30 |
Investigation on the performance and feasibility of RBCC-based access-to-space via multi-objective design optimization
|
Klink, Philipp
|
|
2019
|
157 |
C |
p. 435-454
|
artikel
|
| 31 |
LEAP2 and LCATS industry clusters: A framework for lunar site technology development using global, space-STEM education and global space-industry development networks
|
Ximenes, Samuel W.
|
|
2019
|
157 |
C |
p. 61-72
|
artikel
|
| 32 |
Linear analysis and control of a tethered system with two rigid end bodies
|
Sabey, Nickolas
|
|
2019
|
157 |
C |
p. 517-527
|
artikel
|
| 33 |
Method of heating of the separated parts of launch vehicle during the atmospheric phase of the descent trajectory
|
Trushlyakov, V.
|
|
2019
|
157 |
C |
p. 1-8
|
artikel
|
| 34 |
Multiple-horizon multiple-model predictive control of electromagnetic tethered satellite system
|
AlandiHallaj, MohammadAmin
|
|
2019
|
157 |
C |
p. 250-262
|
artikel
|
| 35 |
NASA's CubeSat Launch Initiative: Enabling broad access to space
|
Crusan, Jason
|
|
2019
|
157 |
C |
p. 51-60
|
artikel
|
| 36 |
Numerical and experimental investigation of an adjustable dual-channel supersonic diffuser
|
Jia, Yicong
|
|
2019
|
157 |
C |
p. 102-110
|
artikel
|
| 37 |
Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules
|
Zhong, Kang
|
|
2019
|
157 |
C |
p. 189-198
|
artikel
|
| 38 |
Optical-aided, autonomous and optimal space rendezvous with a non-cooperative target
|
Volpe, Renato
|
|
2019
|
157 |
C |
p. 528-540
|
artikel
|
| 39 |
Performance characterization of a miniature microwave discharge ion thruster operated with water
|
Nakagawa, Yuichi
|
|
2019
|
157 |
C |
p. 294-299
|
artikel
|
| 40 |
Performance improvement of the μ10 microwave discharge ion thruster by expansion of the plasma production volume
|
Tani, Y.
|
|
2019
|
157 |
C |
p. 425-434
|
artikel
|
| 41 |
Plant cell development and aging may accelerate in microgravity
|
Kordyum, Elizabeth
|
|
2019
|
157 |
C |
p. 157-161
|
artikel
|
| 42 |
REGULUS: A propulsion platform to boost small satellite missions
|
Manente, M.
|
|
2019
|
157 |
C |
p. 241-249
|
artikel
|
| 43 |
Self-cleaning spacesuits for future planetary missions using carbon nanotube technology
|
Manyapu, Kavya K.
|
|
2019
|
157 |
C |
p. 134-144
|
artikel
|
| 44 |
Solar sail trajectory optimization of multi-asteroid rendezvous mission
|
Song, Yu
|
|
2019
|
157 |
C |
p. 111-122
|
artikel
|
| 45 |
Steering law of control moment gyros using artificial potential function approach
|
Seo, Hyun-Ho
|
|
2019
|
157 |
C |
p. 374-389
|
artikel
|
| 46 |
The design and dynamic analysis of a lunar lander with semi-active control
|
Wang, Chen
|
|
2019
|
157 |
C |
p. 145-156
|
artikel
|
| 47 |
The search campaign to identify and image the Philae Lander on the surface of comet 67P/Churyumov-Gerasimenko
|
O'Rourke, L.
|
|
2019
|
157 |
C |
p. 199-214
|
artikel
|
| 48 |
The spacecraft and Science Communicator roles in human missions: Lessons learned from testing various architectures in the Desert RATS field tests
|
Yingst, R. Aileen
|
|
2019
|
157 |
C |
p. 40-50
|
artikel
|
| 49 |
Three-dimensional reconstruction of incident shock/boundary layer interaction using background-oriented schlieren
|
Wang, Chengpeng
|
|
2019
|
157 |
C |
p. 341-349
|
artikel
|
| 50 |
Why planetary and exoplanetary protection differ: The case of long duration genesis missions to habitable but sterile M-dwarf oxygen planets
|
Gros, Claudius
|
|
2019
|
157 |
C |
p. 263-267
|
artikel
|
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