| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A comparison of different unsteady flow control techniques in a highly loaded compressor cascade
|
Zhang, Hongxin
|
|
2019
|
|
6 |
p. 2051-2065
|
artikel
|
| 2 |
A cooperative line-of-sight guidance law for a three-dimensional phantom track generation using unmanned aerial vehicles
|
Lee, Il-Hyoung
|
|
2013
|
|
6 |
p. 897-915
|
artikel
|
| 3 |
Adaptive anti-saturation fault-tolerant control of hypersonic vehicle with actuator faults
|
Sun, Jing-guang
|
|
2019
|
|
6 |
p. 2066-2083
|
artikel
|
| 4 |
Adaptive control of dual-arm space manipulator capturing object
|
Cong, Pei-Chao
|
|
2013
|
|
6 |
p. 992-999
|
artikel
|
| 5 |
Adaptive robust attitude control and active vibration suppression of flexible spacecraft
|
Yu, Z
|
|
2017
|
|
6 |
p. 1076-1087
|
artikel
|
| 6 |
A dynamic model parameter identification method for quadrotors using flight data
|
Lyu, Pin
|
|
2019
|
|
6 |
p. 1990-2002
|
artikel
|
| 7 |
Aerodynamic and static aeroelastic computations of a slender rocket with all-movable canard surface
|
Dongyang, Chen
|
|
2018
|
|
6 |
p. 1103-1119
|
artikel
|
| 8 |
Aerodynamic and static stability characteristics of airfoils in extreme ground effect
|
Nirooei, Mohammadhossein
|
|
2018
|
|
6 |
p. 1134-1148
|
artikel
|
| 9 |
Aerodynamic design optimization for low Reynolds tandem airfoil
|
Chen, Fangzheng
|
|
2018
|
|
6 |
p. 1047-1062
|
artikel
|
| 10 |
A fast robust guidance scheme for a hypersonic vehicle in the diving phase
|
Wang, Jian-Hua
|
|
2018
|
|
6 |
p. 1087-1102
|
artikel
|
| 11 |
Air traffic complexity for a distributed air traffic management system
|
Brázdilová, S L
|
|
2011
|
|
6 |
p. 665-674
|
artikel
|
| 12 |
A methodology for vehicle and mission level comparison of More Electric Aircraft subsystem solutions: Application to the flight control actuation system
|
Chakraborty, Imon
|
|
2015
|
|
6 |
p. 1088-1102
|
artikel
|
| 13 |
An adaptive fading Kalman filter based on Mahalanobis distance
|
Chang, Guobin
|
|
2015
|
|
6 |
p. 1114-1123
|
artikel
|
| 14 |
Analyzing carbon neutral growth and biofuel economic impact for 2017–2025: A case study based on Spanish carriers
|
López Lázaro, Antonio
|
|
2019
|
|
6 |
p. 1943-1959
|
artikel
|
| 15 |
An assessment of thrust vector concepts for twin-engine airplane
|
Vinayagam, AK
|
|
2014
|
|
6 |
p. 960-979
|
artikel
|
| 16 |
A new approach in UAV path planning using Bezier–Dubins continuous curvature path
|
Askari, A
|
|
2016
|
|
6 |
p. 1103-1113
|
artikel
|
| 17 |
A new characteristic analysis method for aero-engine rotor–stator rubbing
|
Yu, Mingyue
|
|
2018
|
|
6 |
p. 1120-1133
|
artikel
|
| 18 |
An experimental investigation of the supersonic turbulent boundary layer subjected to convex curvature
|
Wang, Qian-cheng
|
|
2018
|
|
6 |
p. 1015-1023
|
artikel
|
| 19 |
An initial orbit determination method from relative position increment measurements
|
Song, Jianing
|
|
2018
|
|
6 |
p. 1149-1158
|
artikel
|
| 20 |
An integrated decision-making framework of a heterogeneous aerial robotic swarm for cooperative tasks with minimum requirements
|
Jang, Inmo
|
|
2019
|
|
6 |
p. 2101-2118
|
artikel
|
| 21 |
A novel capture region of retro proportional navigation guidance law for intercepting high-speed nonmaneuvering targets
|
Wang, Huaji
|
|
2018
|
|
6 |
p. 1186-1198
|
artikel
|
| 22 |
A novel 3D feature detection and matching approach for autonomous planetary landing mission
|
Tian, Yang
|
|
2019
|
|
6 |
p. 2241-2249
|
artikel
|
| 23 |
Application and analysis of an improved multiconic method in trajectory design of the lunar south pole return mission
|
Feng, Fei
|
|
2018
|
|
6 |
p. 1063-1076
|
artikel
|
| 24 |
A real-time algorithm for variable-objective motion planning over terrain and threats
|
Karimi, J
|
|
2015
|
|
6 |
p. 1043-1056
|
artikel
|
| 25 |
A simplified linear model and breakup characteristics of power-law sheet formed by a doublet impinging injector
|
Deng, Han-Yu
|
|
2018
|
|
6 |
p. 1035-1046
|
artikel
|
| 26 |
Assessment of aileron tab installation influence on light sport aircraft flutter characteristics
|
Cecrdle, Jiri
|
|
2013
|
|
6 |
p. 1000-1008
|
artikel
|
| 27 |
A stochastic automaton approach to discriminate intermittent from permanent faults
|
Guanqian, Deng
|
|
2014
|
|
6 |
p. 880-888
|
artikel
|
| 28 |
A study on constrained efficient global optimization method for noisy computational fluid dynamics data
|
Bae, Hyo Gil
|
|
2014
|
|
6 |
p. 908-919
|
artikel
|
| 29 |
A theoretical model evaluating leading order vortex decay behind an aircraft
|
Chadwick, E
|
|
2011
|
|
6 |
p. 657-663
|
artikel
|
| 30 |
Attitude aberration correction for space technology experiment and climate exploration (STECE) satellite star tracker
|
Lai, Yuwang
|
|
2015
|
|
6 |
p. 1142-1153
|
artikel
|
| 31 |
Attitude determination sensor for low Earth orbit satellite based on Lorentz force
|
Rezaei, Mohsen
|
|
2019
|
|
6 |
p. 2219-2230
|
artikel
|
| 32 |
A unitized guidance law for over-flight and standoff tracking of a ground target with fixed wing unmanned aerial vehicle
|
Zhang, Min
|
|
2018
|
|
6 |
p. 1024-1034
|
artikel
|
| 33 |
Canard flow improvement in a split canard configuration
|
Davari, Ali R
|
|
2015
|
|
6 |
p. 1076-1087
|
artikel
|
| 34 |
Combustion characteristics of a dual-mode scramjet injecting liquid kerosene by multiple struts
|
Yang, Qingchun
|
|
2015
|
|
6 |
p. 983-992
|
artikel
|
| 35 |
Comparison of hierarchical and non-hierarchical error indicators for adaptive mesh refinement for the Euler equations
|
Becker, Roland
|
|
2013
|
|
6 |
p. 933-943
|
artikel
|
| 36 |
Computational analysis of the aerodynamic performance of a jet-flap airfoil in transonic flow
|
Mantič-Lugo, V
|
|
2012
|
|
6 |
p. 664-678
|
artikel
|
| 37 |
Computational analysis of the aerodynamic performance of a jet-flap airfoil in transonic flow
|
Mantič-Lugo, V
|
|
2012
|
|
6 |
p. 664-678
|
artikel
|
| 38 |
Computational fluid dynamics-based virtual flight simulation of a flying wing micro air vehicle
|
Cai, Hongming
|
|
2016
|
|
6 |
p. 1094-1102
|
artikel
|
| 39 |
Concurrent orbit and attitude estimation using minimum sigma point unscented Kalman filter
|
Kiani, M
|
|
2014
|
|
6 |
p. 801-819
|
artikel
|
| 40 |
Controllability of a square solar sail with movable membrane tips
|
Fu, Bo
|
|
2017
|
|
6 |
p. 1065-1075
|
artikel
|
| 41 |
Cooperative near-space interceptor mid-course guidance law with terminal handover constraints
|
Zhang, Haoqiang
|
|
2019
|
|
6 |
p. 1960-1976
|
artikel
|
| 42 |
Corrugated triangular tabs for supersonic jet control
|
Kumar, P Arun
|
|
2014
|
|
6 |
p. 831-845
|
artikel
|
| 43 |
Coupling in-flight trajectory planning and flocking for multiple autonomous parafoils
|
Rosich, A
|
|
2012
|
|
6 |
p. 691-720
|
artikel
|
| 44 |
Coupling in-flight trajectory planning and flocking for multiple autonomous parafoils
|
Rosich, A
|
|
2012
|
|
6 |
p. 691-720
|
artikel
|
| 45 |
Design of a supervisory algorithm based on failure mode effect criticality analysis for classification of different fault types of attitude determination sensors
|
Abedi, Mostafa
|
|
2019
|
|
6 |
p. 2084-2100
|
artikel
|
| 46 |
Design point analysis of the turbofan-driven turboelectric distributed propulsion system with boundary layer ingestion
|
Liu, Chengyuan
|
|
2016
|
|
6 |
p. 1139-1149
|
artikel
|
| 47 |
Development of low frequency pulse detonation engine with high-G mitigating system for aero-spacecraft propulsion
|
Gong, ShaoWei
|
|
2011
|
|
6 |
p. 645-656
|
artikel
|
| 48 |
Distributed reactive collision avoidance for a swarm of quadrotors
|
Leonard, J
|
|
2017
|
|
6 |
p. 1035-1055
|
artikel
|
| 49 |
Dynamic- and post-stall characteristics of pitching airfoils at extreme conditions
|
Leknys, RR
|
|
2018
|
|
6 |
p. 1171-1185
|
artikel
|
| 50 |
Dynamics and control of a 6-DOF space robot with flexible panels
|
Zhang-Wei, Yu
|
|
2017
|
|
6 |
p. 1022-1034
|
artikel
|
| 51 |
Dynamics of global instabilities in the vaneless diffuser: A numerical approach and its applications
|
Hu, Chenxing
|
|
2018
|
|
6 |
p. 1159-1170
|
artikel
|
| 52 |
Economic and environmental optimization of flight trajectories connecting a city-pair
|
Visser, Hendrikus G
|
|
2014
|
|
6 |
p. 980-993
|
artikel
|
| 53 |
Effect of ambient temperature on piston-type synthetic jet actuator
|
Eri, Qitai
|
|
2018
|
|
6 |
p. 1077-1086
|
artikel
|
| 54 |
Effect of inlet conditions on compressor intermediate duct
|
Gao, Limin
|
|
2015
|
|
6 |
p. 1154-1168
|
artikel
|
| 55 |
Efficient reduced-order modeling of unsteady aerodynamics under light dynamic stall conditions
|
Xiaohua, Li
|
|
2019
|
|
6 |
p. 2141-2151
|
artikel
|
| 56 |
Efficient stall compliance prediction method for trimmed very light aircraft with high-lift devices
|
Van Nguyen, Nhu
|
|
2017
|
|
6 |
p. 1124-1137
|
artikel
|
| 57 |
Efficient trajectory parameterization for environmental optimization of departure flight paths using a genetic algorithm
|
Hartjes, S
|
|
2017
|
|
6 |
p. 1115-1123
|
artikel
|
| 58 |
Efficient use of an allotted airport annual noise budget through minimax optimization of runway allocations
|
Kuiper, Bryan R
|
|
2013
|
|
6 |
p. 1021-1035
|
artikel
|
| 59 |
Eigenstructure assignment-based controllers applied to flexible spacecraft
|
Crespo, J
|
|
2011
|
|
6 |
p. 709-720
|
artikel
|
| 60 |
Equilibrium characteristics and stability analysis of helicopter slung-load system
|
Cao, Yihua
|
|
2017
|
|
6 |
p. 1056-1064
|
artikel
|
| 61 |
Experimental and analytical analysis of aerodynamic lift of an ornithopter at low and high angles of attack
|
Bakhtiari, Abdolbaghi
|
|
2019
|
|
6 |
p. 2023-2031
|
artikel
|
| 62 |
Experimental and numerical investigations on flow fields and performance of dual combustion ramjet
|
Tan, Jianguo
|
|
2014
|
|
6 |
p. 920-929
|
artikel
|
| 63 |
Experimental assessment of the dynamic stiffness of a fault-tolerant fly-by-wire hydraulic actuator
|
Di Rito, G
|
|
2012
|
|
6 |
p. 679-690
|
artikel
|
| 64 |
Experimental assessment of the dynamic stiffness of a fault-tolerant fly-by-wire hydraulic actuator
|
Di Rito, G
|
|
2012
|
|
6 |
p. 679-690
|
artikel
|
| 65 |
Experimental study of the vortex flow and aerodynamic characteristics of a reverse delta wing
|
Lee, T
|
|
2016
|
|
6 |
p. 1126-1138
|
artikel
|
| 66 |
Exploring the aerodynamic characteristics of a blown annular wing for vertical/short take-off and landing applications
|
Saeed, B
|
|
2011
|
|
6 |
p. 689-707
|
artikel
|
| 67 |
FADSat: A system engineering tool for the conceptual design of geostationary Earth orbit satellites platform
|
Mirshams, Mehran
|
|
2019
|
|
6 |
p. 2152-2169
|
artikel
|
| 68 |
Fast terminal sliding mode control based on extended state observer for swing nozzle of anti-aircraft missile
|
Sun, Lianghua
|
|
2015
|
|
6 |
p. 1103-1113
|
artikel
|
| 69 |
Finite-horizon servo SDRE for super-maneuverable aircraft and magnetically-suspended CMGs
|
Geranmehr, Behdad
|
|
2016
|
|
6 |
p. 1075-1093
|
artikel
|
| 70 |
Finite-time antisaturation control for spacecraft rendezvous and docking with safe constraint
|
Wu, Guan-qun
|
|
2019
|
|
6 |
p. 2170-2184
|
artikel
|
| 71 |
Finite-time fault-tolerant attitude tracking control for spacecraft without unwinding
|
Huang, Bing
|
|
2019
|
|
6 |
p. 2119-2130
|
artikel
|
| 72 |
Flow in the near air wake of a modified frigate
|
Bardera, R
|
|
2015
|
|
6 |
p. 1003-1012
|
artikel
|
| 73 |
Flutter of functionally graded open conical shell panels subjected to supersonic air flow
|
Davar, Ali
|
|
2013
|
|
6 |
p. 1036-1052
|
artikel
|
| 74 |
Fuzzy uncertainty analysis in the flutter boundary of an aircraft wing subjected to a thrust force
|
Rezaei, M
|
|
2019
|
|
6 |
p. 2185-2197
|
artikel
|
| 75 |
Hybrid intelligent control for set-point tracking of a flexible manoeuvring system using sigmoid activation function
|
Omar, Muneer E
|
|
2013
|
|
6 |
p. 944-965
|
artikel
|
| 76 |
Hydrogen-fueled scramjet cooling system investigation using combustor and regenerative cooling coupled model
|
Bao, Wen
|
|
2014
|
|
6 |
p. 820-830
|
artikel
|
| 77 |
Identification of the time-varying modal parameters of a spacecraft with flexible appendages using a recursive predictor-based subspace identification algorithm
|
Ni, Zhiyu
|
|
2019
|
|
6 |
p. 2032-2050
|
artikel
|
| 78 |
Immersion- and invariance-based adaptive missile control using filtered signals
|
Lee, K W
|
|
2012
|
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6 |
p. 646-663
|
artikel
|
| 79 |
Immersion- and invariance-based adaptive missile control using filtered signals
|
Lee, K W
|
|
2012
|
|
6 |
p. 646-663
|
artikel
|
| 80 |
Impact angle control based on integral sliding mode manifold and extended state observer
|
Zhang, Xiaojian
|
|
2019
|
|
6 |
p. 2131-2140
|
artikel
|
| 81 |
Influence of chemical models on heat flux for EXPERT and Orion capsules
|
Morsa, Luigi
|
|
2014
|
|
6 |
p. 930-948
|
artikel
|
| 82 |
Influence of leading edge imperfections on the aerodynamic characteristics of NACA 632-215 laminar aerofoils at low Reynolds numbers
|
Ayuso, L
|
|
2014
|
|
6 |
p. 859-868
|
artikel
|
| 83 |
Integrated flight/thrust vectoring control for jet-powered unmanned aerial vehicles with ACHEON propulsion
|
Cen, Zhaohui
|
|
2015
|
|
6 |
p. 1057-1075
|
artikel
|
| 84 |
Integrated guidance and control design considering system uncertainty
|
Chao, Tao
|
|
2019
|
|
6 |
p. 2278-2290
|
artikel
|
| 85 |
Investigations of rotating instability and fluctuating tip clearance flow in a low-speed axial compressor
|
Wang, Hao
|
|
2016
|
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6 |
p. 981-994
|
artikel
|
| 86 |
Leakage analysis and ground tests of knife edge indium seal to lunar sample return devices
|
Zhang, Bin
|
|
2019
|
|
6 |
p. 2010-2022
|
artikel
|
| 87 |
Matrix weighted multisensor data fusion for INS/GNSS/CNS integration
|
Hu, Gaoge
|
|
2016
|
|
6 |
p. 1011-1026
|
artikel
|
| 88 |
Model-free simulations for compressible mixing layer
|
Javed, Afroz
|
|
2013
|
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6 |
p. 977-991
|
artikel
|
| 89 |
Modeling of unsteady aerodynamic characteristics at high angles of attack
|
Hao, Dong
|
|
2019
|
|
6 |
p. 2291-2301
|
artikel
|
| 90 |
Multi-field coupling dynamic characteristics based on Kriging interpolation method
|
Yang, Wenjun
|
|
2017
|
|
6 |
p. 1088-1099
|
artikel
|
| 91 |
Multilevel finite element modeling and coupling vibration analysis of the drum in blade–disk–drum assembly
|
Chen, Yugang
|
|
2017
|
|
6 |
p. 998-1011
|
artikel
|
| 92 |
Multiphase trajectory optimization for gun-launched glide guided projectiles
|
Chen, Qi
|
|
2016
|
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6 |
p. 995-1010
|
artikel
|
| 93 |
Multiple-input describing function technique applied to design a single channel ON-OFF controller for a spinning flight vehicle
|
Nobahari, H
|
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2012
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6 |
p. 631-645
|
artikel
|
| 94 |
Multiple-input describing function technique applied to design a single channel ON-OFF controller for a spinning flight vehicle
|
Nobahari, H
|
|
2012
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6 |
p. 631-645
|
artikel
|
| 95 |
Network analysis of a coolant flow performance for the combined impingement and film cooled first-stage of high pressure gas turbine nozzle guide vane
|
Reddy Kukutla, Pol
|
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2019
|
|
6 |
p. 1977-1989
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artikel
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| 96 |
Neural network based dynamic model and gust identification system for the Jetstream G-NFLA
|
Antonakis, Aristeidis
|
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2017
|
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6 |
p. 1138-1153
|
artikel
|
| 97 |
Nonlinear adaptive filter backstepping flight control for reentry vehicle with input constraint and external disturbances
|
Zong, Q
|
|
2014
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6 |
p. 889-907
|
artikel
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| 98 |
Non-linear solution to the maximum height orbit transfer guidance problem
|
Afshari, H H
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2012
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6 |
p. 620-630
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artikel
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| 99 |
Non-linear solution to the maximum height orbit transfer guidance problem
|
Afshari, H H
|
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2012
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6 |
p. 620-630
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artikel
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| 100 |
Numerical investigation of fragmentation initiation threshold for sphere impacting on thin wall at hypervelocity
|
Zhang, Xiaotian
|
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2016
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6 |
p. 967-980
|
artikel
|
| 101 |
Numerical study on vibration stress of rotating fan blade under aerodynamic load at critical speed
|
Kou, Hai-jun
|
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2016
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6 |
p. 1044-1058
|
artikel
|
| 102 |
Occasion determination method of low Earth orbit satellites meeting the narrow-beam signal
|
Ma, Yiwei
|
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2019
|
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6 |
p. 2198-2206
|
artikel
|
| 103 |
On-line guidance with trajectory constraints for terminal area energy management of re-entry vehicles
|
Morani, G
|
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2011
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6 |
p. 631-643
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artikel
|
| 104 |
On measuring key parameters of an electro-impulse deicing system
|
Du, Qian
|
|
2019
|
|
6 |
p. 2321-2328
|
artikel
|
| 105 |
Optimal design of the volute for a turbocharger radial flow compressor
|
Mojaddam, Mohammad
|
|
2015
|
|
6 |
p. 993-1002
|
artikel
|
| 106 |
Optimal formation control with limited communication for multi-unmanned aerial vehicle in an obstacle-laden environment
|
Ai, Xiao Lin
|
|
2017
|
|
6 |
p. 979-997
|
artikel
|
| 107 |
Optimal online trajectory generation for a flying robot for terrain following purposes using neural network
|
Kosari, Amirreza
|
|
2015
|
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6 |
p. 1124-1141
|
artikel
|
| 108 |
Optimal sample-data control for free-floating space robot with uncertain inertial parameters
|
Yang, Fan
|
|
2019
|
|
6 |
p. 2302-2320
|
artikel
|
| 109 |
Orbital transfer strategy using only-accelerating maneuvers
|
Luo, Tong
|
|
2019
|
|
6 |
p. 2003-2009
|
artikel
|
| 110 |
Oscillating aerofoil and perpendicular vortex interaction
|
Gibertini, G
|
|
2014
|
|
6 |
p. 846-858
|
artikel
|
| 111 |
Parallel intelligent algorithm analysis of optimization arrangement on mistuned blades based on compute unified device architecture
|
Zhao, Tianyu
|
|
2019
|
|
6 |
p. 2207-2218
|
artikel
|
| 112 |
Parametric study on self-sustained oscillation characteristics of cavity flameholders in supersonic flows
|
Sun, M B
|
|
2011
|
|
6 |
p. 597-618
|
artikel
|
| 113 |
Partially independent control scheme for spacecraft rendezvous in near-circular orbits
|
Wan, Neng
|
|
2019
|
|
6 |
p. 2250-2263
|
artikel
|
| 114 |
Research on spacecraft design for ORS based on the systems theory
|
Huang, Wen-bo
|
|
2014
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