| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active damping control of flexible appendages for spacecraft
|
Zhang, Yizhe
|
|
|
75 |
C |
p. 237-244
|
artikel
|
| 2 |
Addendum to “Magnetic attitude control of bias momentum spacecraft by bounded linear feedback” [Aerosp. Sci. Technol. 70 (2017) 419–427]
|
Luo, Weiwei
|
|
|
75 |
C |
p. 386-387
|
artikel
|
| 3 |
A fast-prediction surrogate model for large datasets
|
Hwang, John T.
|
|
|
75 |
C |
p. 74-87
|
artikel
|
| 4 |
Aircraft icing: An ongoing threat to aviation safety
|
Cao, Yihua
|
|
|
75 |
C |
p. 353-385
|
artikel
|
| 5 |
A methodology for hybrid simulation of rarefield and continuum flow regimes
|
Ladeinde, Foluso
|
|
|
75 |
C |
p. 115-127
|
artikel
|
| 6 |
An approach and landing guidance design for reusable launch vehicle based on adaptive predictor–corrector technique
|
Li, Maomao
|
|
|
75 |
C |
p. 13-23
|
artikel
|
| 7 |
A numerical method for the ballistic performance prediction of the sandwiched open cell aluminum foam under hypervelocity impact
|
Zhang, Xiaotian
|
|
|
75 |
C |
p. 254-260
|
artikel
|
| 8 |
A simple analytical model to describe the impact of wing on the flowfield over the tail in subsonic flow
|
Davari, Ali R.
|
|
|
75 |
C |
p. 88-98
|
artikel
|
| 9 |
Distributed almost global finite-time attitude consensus of multiple spacecraft without velocity measurements
|
Gui, Haichao
|
|
|
75 |
C |
p. 284-296
|
artikel
|
| 10 |
Dynamic analysis and control application of vibration isolation system with magnetic suspension on satellites
|
Zhang, Yao
|
|
|
75 |
C |
p. 99-114
|
artikel
|
| 11 |
Editorial Board
|
|
|
|
75 |
C |
p. ii
|
artikel
|
| 12 |
Elastic properties of a novel cellular structure with trapezoidal beams
|
Liu, Weidong
|
|
|
75 |
C |
p. 315-328
|
artikel
|
| 13 |
Experimental and numerical investigations of freejet and direct-connect dual-mode scramjet
|
Xiao, Baoguo
|
|
|
75 |
C |
p. 297-303
|
artikel
|
| 14 |
Experimental and numerical study on residual strength of aircraft carbon/epoxy composite after lightning strike
|
Wang, F.S.
|
|
|
75 |
C |
p. 304-314
|
artikel
|
| 15 |
Inverse dynamics particle swarm optimization applied to constrained minimum-time maneuvers using reaction wheels
|
Spiller, Dario
|
|
|
75 |
C |
p. 1-12
|
artikel
|
| 16 |
Low energy actuation technique of bistable composites for aircraft morphing
|
Nicassio, F.
|
|
|
75 |
C |
p. 35-46
|
artikel
|
| 17 |
MFVS/MIMU integrated 6-DOF autonomous navigation in known environments with extremely simple landmarks
|
Shi, Shuai
|
|
|
75 |
C |
p. 329-341
|
artikel
|
| 18 |
Modification of hypersonic waveriders by vorticity-based boundary layer displacement thickness determination method
|
Liu, Wen
|
|
|
75 |
C |
p. 200-214
|
artikel
|
| 19 |
Near optimal finite-time terminal controllers for space trajectories via SDRE-based approach using dynamic programming
|
Sharma, Rajnish
|
|
|
75 |
C |
p. 128-138
|
artikel
|
| 20 |
Nonlinear aircraft system identification using artificial neural networks enhanced by empirical mode decomposition
|
Bagherzadeh, Seyed Amin
|
|
|
75 |
C |
p. 155-171
|
artikel
|
| 21 |
Numerical and experimental investigations of single-element and double-element injectors using gaseous oxygen/gaseous methane
|
Yu, Nanjia
|
|
|
75 |
C |
p. 24-34
|
artikel
|
| 22 |
On novel adaptive saturated deployment control of tethered satellite system with guaranteed output tracking prescribed performance
|
Wei, Caisheng
|
|
|
75 |
C |
p. 58-73
|
artikel
|
| 23 |
On the influence of optimization algorithm and initial design on wing aerodynamic shape optimization
|
Yu, Yin
|
|
|
75 |
C |
p. 183-199
|
artikel
|
| 24 |
Optimal fuel consumption finite-thrust orbital hopping of aeroassisted spacecraft
|
Chai, Runqi
|
|
|
75 |
C |
p. 172-182
|
artikel
|
| 25 |
Quasi-1D modeling of heat release for the study of longitudinal combustion instability
|
Frezzotti, Maria L.
|
|
|
75 |
C |
p. 261-270
|
artikel
|
| 26 |
Robust virtual target guidance for the fixed-trim vehicle under multi-constraints
|
Zhang, Qingzhen
|
|
|
75 |
C |
p. 271-283
|
artikel
|
| 27 |
Scramjet performance for ideal combustion processes
|
Vanyai, Tristan
|
|
|
75 |
C |
p. 215-226
|
artikel
|
| 28 |
Solid fuel ramjet fuel optimization for maximum thrust to drag ratio and impulse density subject to geometric restraints on missile outer mold line
|
McDonald, Brian
|
|
|
75 |
C |
p. 47-57
|
artikel
|
| 29 |
Spacecraft attitude fault-tolerant control based on iterative learning observer and control allocation
|
Hu, Qinglei
|
|
|
75 |
C |
p. 245-253
|
artikel
|
| 30 |
Time efficient sliding mode controller based on Bang–Bang logic for satellite attitude control
|
Li, You
|
|
|
75 |
C |
p. 342-352
|
artikel
|
| 31 |
Turbulence characteristics in corner separation in a highly loaded linear compressor cascade
|
Yan, Hao
|
|
|
75 |
C |
p. 139-154
|
artikel
|
| 32 |
Vibroacoustic behavior of orthotropic aerospace composite structure in the subsonic flow considering the Third order Shear Deformation Theory
|
Talebitooti, R.
|
|
|
75 |
C |
p. 227-236
|
artikel
|
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