| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Adaptive multipath mitigation tracking system for GPS receiver
|
Mao, Wei-Lung
|
|
2013
|
30 |
1 |
p. 66-78
13 p.
|
artikel
|
| 2 |
Aerodynamic parameter identification for symmetric projectiles: An improved gradient based method
|
Burchett, Bradley T.
|
|
2013
|
30 |
1 |
p. 119-127
9 p.
|
artikel
|
| 3 |
An analytic solution to Wahbaʼs problem
|
Yang, Yaguang
|
|
2013
|
30 |
1 |
p. 46-49
4 p.
|
artikel
|
| 4 |
Backstepping based adaptive sliding mode control for spacecraft attitude maneuvers
|
Cong, Binglong
|
|
2013
|
30 |
1 |
p. 1-7
7 p.
|
artikel
|
| 5 |
Calibration of antenna arrays for aeronautical vehicles on ground
|
Elbir, Ahmet M.
|
|
2013
|
30 |
1 |
p. 18-25
8 p.
|
artikel
|
| 6 |
Coning motion instability of spinning missiles induced by hinge moment
|
Zhou, Wei
|
|
2013
|
30 |
1 |
p. 239-245
7 p.
|
artikel
|
| 7 |
Detached-eddy simulations on massively separated flows over a 76/40° double-delta wing
|
Sun, Dong
|
|
2013
|
30 |
1 |
p. 33-45
13 p.
|
artikel
|
| 8 |
Development of optimal and robust predictive guidance technique for Mars aerocapture
|
Kozynchenko, Alexander I.
|
|
2013
|
30 |
1 |
p. 150-162
13 p.
|
artikel
|
| 9 |
Editorial Board
|
|
|
2013
|
30 |
1 |
p. IFC-
1 p.
|
artikel
|
| 10 |
Effect of a block on flow oscillations near evaporating solid fuel surface
|
Koo, Heeseok
|
|
2013
|
30 |
1 |
p. 269-277
9 p.
|
artikel
|
| 11 |
Evaluation system for effective thermophysical properties of anisotropic composite material
|
Bai, Dan
|
|
2013
|
30 |
1 |
p. 94-101
8 p.
|
artikel
|
| 12 |
Experimental analysis of the pressure–velocity correlations of external unsteady flow over rocket launchers
|
Marié, S.
|
|
2013
|
30 |
1 |
p. 83-93
11 p.
|
artikel
|
| 13 |
Extended estimation method for lateral flight technical error of perturbed system in performance based navigation
|
Zhao, Hongsheng
|
|
2013
|
30 |
1 |
p. 278-285
8 p.
|
artikel
|
| 14 |
Fast convergence of orbit determination using geomagnetic field measurement in Target Pointing Satellite
|
Cheon, Yee-Jin
|
|
2013
|
30 |
1 |
p. 315-322
8 p.
|
artikel
|
| 15 |
Heat capacity estimation of the thermal buffer mass for temperature control of satellite electronic components in periodic operation
|
Kim, T.Y.
|
|
2013
|
30 |
1 |
p. 286-292
7 p.
|
artikel
|
| 16 |
Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow
|
Camilo, Elizangela
|
|
2013
|
30 |
1 |
p. 163-174
12 p.
|
artikel
|
| 17 |
Influence of the connection section on the aerodynamic performance of the tandem waverider in a wide-speed range
|
Li, Shi-bin
|
|
2013
|
30 |
1 |
p. 50-65
16 p.
|
artikel
|
| 18 |
Initial position and attitude determination of lunar rovers by INS/CNS integration
|
Ning, Xiaolin
|
|
2013
|
30 |
1 |
p. 323-332
10 p.
|
artikel
|
| 19 |
Modeling and controller design of inner-formation flying system with two proof-masses
|
Dang, Zhaohui
|
|
2013
|
30 |
1 |
p. 8-17
10 p.
|
artikel
|
| 20 |
Multi-discipline optimization of sandwich cylinders under a point force excitation
|
Yuan, Chongxin
|
|
2013
|
30 |
1 |
p. 183-191
9 p.
|
artikel
|
| 21 |
Multiobjective design optimization of the performance for the cavity flameholder in supersonic flows
|
Huang, Wei
|
|
2013
|
30 |
1 |
p. 246-254
9 p.
|
artikel
|
| 22 |
New concept of dynamic flight simulator, Part I
|
Dourado, Antônio O.
|
|
2013
|
30 |
1 |
p. 79-82
4 p.
|
artikel
|
| 23 |
Numerical analysis and characterization of the dissociated flowfield inside a 1.6 MW arc-heated wind tunnel facility
|
Ground, Cody
|
|
2013
|
30 |
1 |
p. 306-314
9 p.
|
artikel
|
| 24 |
Numerical analysis of the effect of vortex control mechanism on longitudinal aerodynamics of lifting body
|
Badarudin Mohamad Badry, Ahmad
|
|
2013
|
30 |
1 |
p. 232-238
7 p.
|
artikel
|
| 25 |
On using neural networks in UAV structural design for CFD data fitting and classification
|
Mazhar, Farrukh
|
|
2013
|
30 |
1 |
p. 210-225
16 p.
|
artikel
|
| 26 |
Reflectivity-controlled solar sail formation flying for magnetosphere mission
|
Mu, Junshan
|
|
2013
|
30 |
1 |
p. 339-348
10 p.
|
artikel
|
| 27 |
Research on application of single moving mass in the reentry warhead maneuver
|
Gao, Changsheng
|
|
2013
|
30 |
1 |
p. 108-118
11 p.
|
artikel
|
| 28 |
Retrieval of aerosol properties by using Low Earth Orbit
|
Ortore, Emiliano
|
|
2013
|
30 |
1 |
p. 333-338
6 p.
|
artikel
|
| 29 |
Robust fixed structure output feedback flight control law synthesis and analysis using singular structured value
|
Siqueira, Daniel
|
|
2013
|
30 |
1 |
p. 102-107
6 p.
|
artikel
|
| 30 |
Rule derivation for arrival aircraft sequencing
|
Andreeva-Mori, Adriana
|
|
2013
|
30 |
1 |
p. 200-209
10 p.
|
artikel
|
| 31 |
Shape adjustment of cable mesh antennas using sequential quadratic programming
|
Du, Jingli
|
|
2013
|
30 |
1 |
p. 26-32
7 p.
|
artikel
|
| 32 |
Shape design optimization of embedded engine inlets for N2B hybrid wing-body configuration
|
Kim, Hyoungjin
|
|
2013
|
30 |
1 |
p. 128-149
22 p.
|
artikel
|
| 33 |
Simulating unsteady aerodynamics of helicopter rotor with panel/viscous vortex particle method
|
Tan, Jian-feng
|
|
2013
|
30 |
1 |
p. 255-268
14 p.
|
artikel
|
| 34 |
Structural dynamics modeling of rectangular rotor blades
|
Truong, Khiem-Van
|
|
2013
|
30 |
1 |
p. 293-305
13 p.
|
artikel
|
| 35 |
Study on shock wave-vortex ring interaction by the micro vortex generator controlled ramp flow with turbulent inflow
|
Yan, Yonghua
|
|
2013
|
30 |
1 |
p. 226-231
6 p.
|
artikel
|
| 36 |
Thermal effects on the sound transmission through aerospace composite structures
|
Chronopoulos, D.
|
|
2013
|
30 |
1 |
p. 192-199
8 p.
|
artikel
|
| 37 |
Thermal post-buckling and snap-through instabilities of FGM panels in hypersonic flows
|
Lee, Chang-Yull
|
|
2013
|
30 |
1 |
p. 175-182
8 p.
|
artikel
|
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