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                             37 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 Adaptive block dynamic surface control for integrated missile guidance and autopilot Hou, Mingzhe
2013
26 3 p. 741-750
10 p.
artikel
2 Adaptive path planning for unmanned aerial vehicles based on bi-level programming and variable planning time interval Liu, Wei
2013
26 3 p. 646-660
15 p.
artikel
3 Aircraft-on-ground path following control by dynamical adaptive backstepping Chen, Bihua
2013
26 3 p. 668-675
8 p.
artikel
4 A novel approach of testability modeling and analysis for PHM systems based on failure evolution mechanism Tan, Xiaodong
2013
26 3 p. 766-776
11 p.
artikel
5 A novel autonomous self-assembly distributed swarm flying robot Wei, Hongxing
2013
26 3 p. 791-800
10 p.
artikel
6 A novel LAAS pseudo-range error over-bound method based on improved pseudo-range error distribution model Xue, Rui
2013
26 3 p. 638-645
8 p.
artikel
7 A robust solution for hesitate phenomenon in pick up process of aerospace electromagnetic relay Ye, Xuerong
2013
26 3 p. 697-704
8 p.
artikel
8 A satellite schedulability prediction algorithm for EO SPS Li, Jun
2013
26 3 p. 705-716
12 p.
artikel
9 Closed-loop dynamic control allocation for aircraft with multiple actuators Gai, Wendong
2013
26 3 p. 676-686
11 p.
artikel
10 Codes cross-correlation analysis and data/pilot code pairs optimization for Galileo E1 OS and GPS L1C Yang, Zaixiu
2013
26 3 p. 751-765
15 p.
artikel
11 Composite control method for stabilizing spacecraft attitude in terms of Rodrigues parameters Sun, Haibin
2013
26 3 p. 687-696
10 p.
artikel
12 Contents 2013
26 3 p. i-ii
nvt p.
artikel
13 Design of face-hobbed spiral bevel gears with reduced maximum tooth contact pressure and transmission errors Simon, Vilmos
2013
26 3 p. 777-790
14 p.
artikel
14 Effect of tip geometry and tip clearance on aerodynamic performance of a linear compressor cascade Zhong, Jingjun
2013
26 3 p. 583-593
11 p.
artikel
15 Fatigue crack propagation of new aluminum lithium alloy bonded with titanium alloy strap Sun, Zhenqi
2013
26 3 p. 601-605
5 p.
artikel
16 Friction compensation for low velocity control of hydraulic flight motion simulator: A simple adaptive robust approach Yao, Jianyong
2013
26 3 p. 814-822
9 p.
artikel
17 Gaseous plume flows in space propulsion Wang, Limei
2013
26 3 p. 522-528
7 p.
artikel
18 Hybrid calibration method for six-component force/torque transducers of wind tunnel balance based on support vector machines Ma, Yingkun
2013
26 3 p. 554-562
9 p.
artikel
19 IFC (Editorial Board) 2013
26 3 p. IFC-
1 p.
artikel
20 Improvement of Baldwin–Lomax turbulence model for supersonic complex flows Zhao, Rui
2013
26 3 p. 529-534
6 p.
artikel
21 Influence of thermal inhibitor position and temperature on vortex-shedding-driven pressure oscillations Su, Wanxing
2013
26 3 p. 544-553
10 p.
artikel
22 Infrared radiation signature of exhaust plume from solid propellants with different energy characteristics Wang, Weichen
2013
26 3 p. 594-600
7 p.
artikel
23 Investigations on damage resistance of carbon fiber composite panels toughened using veils Zhu, Lingang
2013
26 3 p. 807-813
7 p.
artikel
24 Mechanistic identification of cutting force coefficients in bull-nose milling process Gao, Ge
2013
26 3 p. 823-830
8 p.
artikel
25 Model-based robustness testing for avionics-embedded software Yang, Shunkun
2013
26 3 p. 730-740
11 p.
artikel
26 Numerical analysis on noise of rotor with unconventional blade tips based on CFD/Kirchhoff method Wang, Bo
2013
26 3 p. 572-582
11 p.
artikel
27 Numerical study of unsteady starting characteristics of a hypersonic inlet Wang, Weixing
2013
26 3 p. 563-571
9 p.
artikel
28 Panel/full-span free-wake coupled method for unsteady aerodynamics of helicopter rotor blade Tan, Jianfeng
2013
26 3 p. 535-543
9 p.
artikel
29 Real-time fault detection method based on belief rule base for aircraft navigation system Zhao, Xin
2013
26 3 p. 717-729
13 p.
artikel
30 Relay selection based on MAP estimation for cooperative communication with outdated channel state information Ding, Wenrui
2013
26 3 p. 661-667
7 p.
artikel
31 Reliability analysis of aero-engine blades considering nonlinear strength degeneration Lin, Jiewei
2013
26 3 p. 631-637
7 p.
artikel
32 Review of shock wave detection method in CFD post-processing Wu, Ziniu
2013
26 3 p. 501-513
13 p.
artikel
33 Safety estimation of structural systems via interval analysis Wang, Xiaojun
2013
26 3 p. 614-623
10 p.
artikel
34 Stability analysis of an aeroelastic system with friction Tan, Tiancai
2013
26 3 p. 624-630
7 p.
artikel
35 Static aeroelastic analysis of very flexible wings based on non-planar vortex lattice method Xie, Changchuan
2013
26 3 p. 514-521
8 p.
artikel
36 Study on ballistic penetration resistance of titanium alloy TC4, Part II: Numerical analysis Zhang, Tao
2013
26 3 p. 606-613
8 p.
artikel
37 Yield anisotropy and tension/compression asymmetry of a Ni3Al based intermetallic alloy Chen, Lei
2013
26 3 p. 801-806
6 p.
artikel
                             37 gevonden resultaten
 
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