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                             32 results found
no title author magazine year volume issue page(s) type
1 Active damping control of flexible appendages for spacecraft Zhang, Yizhe

75 C p. 237-244
article
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
article
3 A fast-prediction surrogate model for large datasets Hwang, John T.

75 C p. 74-87
article
4 Aircraft icing: An ongoing threat to aviation safety Cao, Yihua

75 C p. 353-385
article
5 A methodology for hybrid simulation of rarefield and continuum flow regimes Ladeinde, Foluso

75 C p. 115-127
article
6 An approach and landing guidance design for reusable launch vehicle based on adaptive predictor–corrector technique Li, Maomao

75 C p. 13-23
article
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
article
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
article
9 Distributed almost global finite-time attitude consensus of multiple spacecraft without velocity measurements Gui, Haichao

75 C p. 284-296
article
10 Dynamic analysis and control application of vibration isolation system with magnetic suspension on satellites Zhang, Yao

75 C p. 99-114
article
11 Editorial Board
75 C p. ii
article
12 Elastic properties of a novel cellular structure with trapezoidal beams Liu, Weidong

75 C p. 315-328
article
13 Experimental and numerical investigations of freejet and direct-connect dual-mode scramjet Xiao, Baoguo

75 C p. 297-303
article
14 Experimental and numerical study on residual strength of aircraft carbon/epoxy composite after lightning strike Wang, F.S.

75 C p. 304-314
article
15 Inverse dynamics particle swarm optimization applied to constrained minimum-time maneuvers using reaction wheels Spiller, Dario

75 C p. 1-12
article
16 Low energy actuation technique of bistable composites for aircraft morphing Nicassio, F.

75 C p. 35-46
article
17 MFVS/MIMU integrated 6-DOF autonomous navigation in known environments with extremely simple landmarks Shi, Shuai

75 C p. 329-341
article
18 Modification of hypersonic waveriders by vorticity-based boundary layer displacement thickness determination method Liu, Wen

75 C p. 200-214
article
19 Near optimal finite-time terminal controllers for space trajectories via SDRE-based approach using dynamic programming Sharma, Rajnish

75 C p. 128-138
article
20 Nonlinear aircraft system identification using artificial neural networks enhanced by empirical mode decomposition Bagherzadeh, Seyed Amin

75 C p. 155-171
article
21 Numerical and experimental investigations of single-element and double-element injectors using gaseous oxygen/gaseous methane Yu, Nanjia

75 C p. 24-34
article
22 On novel adaptive saturated deployment control of tethered satellite system with guaranteed output tracking prescribed performance Wei, Caisheng

75 C p. 58-73
article
23 On the influence of optimization algorithm and initial design on wing aerodynamic shape optimization Yu, Yin

75 C p. 183-199
article
24 Optimal fuel consumption finite-thrust orbital hopping of aeroassisted spacecraft Chai, Runqi

75 C p. 172-182
article
25 Quasi-1D modeling of heat release for the study of longitudinal combustion instability Frezzotti, Maria L.

75 C p. 261-270
article
26 Robust virtual target guidance for the fixed-trim vehicle under multi-constraints Zhang, Qingzhen

75 C p. 271-283
article
27 Scramjet performance for ideal combustion processes Vanyai, Tristan

75 C p. 215-226
article
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
article
29 Spacecraft attitude fault-tolerant control based on iterative learning observer and control allocation Hu, Qinglei

75 C p. 245-253
article
30 Time efficient sliding mode controller based on Bang–Bang logic for satellite attitude control Li, You

75 C p. 342-352
article
31 Turbulence characteristics in corner separation in a highly loaded linear compressor cascade Yan, Hao

75 C p. 139-154
article
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
article
                             32 results found
 
 Koninklijke Bibliotheek - National Library of the Netherlands