| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A CFD–CSD coupled-analysis of HART-II rotor vibration reduction using gurney flaps
|
Min, Byung-Young
|
|
2016
|
48 |
C |
p. 308-321
14 p.
|
artikel
|
| 2 |
A general evaluation criterion for the coverage performance of LEO constellations
|
Li, Yongjun
|
|
2016
|
48 |
C |
p. 94-101
8 p.
|
artikel
|
| 3 |
Aircraft localization using a passive acoustic method. Experimental test
|
Martín, Sara R.
|
|
2016
|
48 |
C |
p. 246-253
8 p.
|
artikel
|
| 4 |
Analysis of dynamic characteristics of the rigid body/elastic body coupling of air-breathing hypersonic vehicles
|
Zhang, Dong
|
|
2016
|
48 |
C |
p. 328-341
14 p.
|
artikel
|
| 5 |
A novel decentralized relative navigation algorithm for spacecraft formation flying
|
Wang, Xiaogang
|
|
2016
|
48 |
C |
p. 28-36
9 p.
|
artikel
|
| 6 |
A parametric study on the stress analysis and transient response of thick-laminated-faced cylindrical sandwich panels with transversely flexible core
|
Khanjani, M.
|
|
2016
|
48 |
C |
p. 1-20
20 p.
|
artikel
|
| 7 |
A POMDP approach for scheduling the usage of airborne electronic countermeasures in air operations
|
Song, Haifang
|
|
2016
|
48 |
C |
p. 86-93
8 p.
|
artikel
|
| 8 |
Attitude control of an underactuated spacecraft using tube-based MPC approach
|
Mirshams, M.
|
|
2016
|
48 |
C |
p. 140-145
6 p.
|
artikel
|
| 9 |
A UKF based design method for lunar free-return trajectories
|
Zhang, Hongli
|
|
2016
|
48 |
C |
p. 272-280
9 p.
|
artikel
|
| 10 |
Coplanar ground-track adjustment using time difference
|
Zhang, Gang
|
|
2016
|
48 |
C |
p. 21-27
7 p.
|
artikel
|
| 11 |
Deployment analysis considering the cable-net tension effect for deployable antennas
|
Zhang, Yiqun
|
|
2016
|
48 |
C |
p. 193-202
10 p.
|
artikel
|
| 12 |
Desensitized optimal trajectory for landing on small bodies with reduced landing error
|
Hu, Haijing
|
|
2016
|
48 |
C |
p. 178-185
8 p.
|
artikel
|
| 13 |
Editorial Board
|
|
|
2016
|
48 |
C |
p. IFC-
1 p.
|
artikel
|
| 14 |
Effective approach for actually uncorrelated angular vibration pattern design of a ring laser angle sensor
|
Shim, Kyu-Min
|
|
2016
|
48 |
C |
p. 254-260
7 p.
|
artikel
|
| 15 |
Effect of a pusher propeller on a delta wing
|
Traub, L.W.
|
|
2016
|
48 |
C |
p. 115-121
7 p.
|
artikel
|
| 16 |
Entry trajectory planning based on three-dimensional acceleration profile guidance
|
Zhang, Yuan-long
|
|
2016
|
48 |
C |
p. 131-139
9 p.
|
artikel
|
| 17 |
Flow and heat transfer of nanofluid in an asymmetric channel with expanding and contracting walls suspended by carbon nanotubes: A numerical investigation
|
Ahmed, Naveed
|
|
2016
|
48 |
C |
p. 53-60
8 p.
|
artikel
|
| 18 |
Inertial/celestial-based fuzzy adaptive unscented Kalman filter with Covariance Intersection algorithm for satellite attitude determination
|
Wang, Xiaochu
|
|
2016
|
48 |
C |
p. 214-222
9 p.
|
artikel
|
| 19 |
INS/VNS/CNS integrated navigation method for planetary rovers
|
Ning, Xiaolin
|
|
2016
|
48 |
C |
p. 102-114
13 p.
|
artikel
|
| 20 |
Interaction of multiple vortices over a double delta wing
|
Zhang, X.
|
|
2016
|
48 |
C |
p. 291-307
17 p.
|
artikel
|
| 21 |
Measurements and modelling of wall heat fluxes in rocket combustion chamber with porous injector head
|
Zhukov, Victor P.
|
|
2016
|
48 |
C |
p. 67-74
8 p.
|
artikel
|
| 22 |
Moment-independent importance measure of correlated input variable and its state dependent parameter solution
|
Li, Luyi
|
|
2016
|
48 |
C |
p. 281-290
10 p.
|
artikel
|
| 23 |
Multi-Bernoulli smoother for multi-target tracking
|
Li, Dong
|
|
2016
|
48 |
C |
p. 234-245
12 p.
|
artikel
|
| 24 |
Multi-constrained suboptimal powered descent guidance for lunar pinpoint soft landing
|
Zhang, Bo
|
|
2016
|
48 |
C |
p. 203-213
11 p.
|
artikel
|
| 25 |
New 3-D ice accretion method of hovering rotor including effects of centrifugal force
|
Zhao, Guo-qing
|
|
2016
|
48 |
C |
p. 122-130
9 p.
|
artikel
|
| 26 |
Nonlinear radiation effects on squeezing flow of a Casson fluid between parallel disks
|
Mohyud-Din, Syed Tauseef
|
|
2016
|
48 |
C |
p. 186-192
7 p.
|
artikel
|
| 27 |
Numerical study of the aerodynamic characteristics of high-lift droop nose with the deflection of fowler flap and spoiler
|
Wang, Wenhu
|
|
2016
|
48 |
C |
p. 75-85
11 p.
|
artikel
|
| 28 |
Optimal design of the Integrated Modular Power Electronics Cabinet
|
Giraud, X.
|
|
2016
|
48 |
C |
p. 37-52
16 p.
|
artikel
|
| 29 |
Optimal guidance law design for guided munitions based on segmental linear functions
|
Dou, Lei
|
|
2016
|
48 |
C |
p. 61-66
6 p.
|
artikel
|
| 30 |
Research on thermal protection by opposing jet and transpiration for high speed vehicle
|
Rong, Yisheng
|
|
2016
|
48 |
C |
p. 322-327
6 p.
|
artikel
|
| 31 |
Sequential multilayer fusion based assessment model for spacecraft launch success ratio
|
Yang, Shan
|
|
2016
|
48 |
C |
p. 223-233
11 p.
|
artikel
|
| 32 |
Simulation validation of static and forced motion flow physics of a canard configured TransCruiser
|
Ghoreyshi, Mehdi
|
|
2016
|
48 |
C |
p. 158-177
20 p.
|
artikel
|
| 33 |
The GA-ANN expert system for mass-model classification of TSTO surrogates
|
Sarosh, Ali
|
|
2016
|
48 |
C |
p. 146-157
12 p.
|
artikel
|
| 34 |
Three spacecraft formation control by means of electrostatic forces
|
Felicetti, Leonard
|
|
2016
|
48 |
C |
p. 261-271
11 p.
|
artikel
|
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