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 |
|
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 |
|
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 |
|
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 |
|
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 |
|
2012 |
|
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 |
|
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 |
|
2019 |
|
6 |
p. 1977-1989 |
artikel |
96 |
Neural network based dynamic model and gust identification system for the Jetstream G-NFLA
|
Antonakis, Aristeidis |
|
2017 |
|
6 |
p. 1138-1153 |
artikel |
97 |
Nonlinear adaptive filter backstepping flight control for reentry vehicle with input constraint and external disturbances
|
Zong, Q |
|
2014 |
|
6 |
p. 889-907 |
artikel |
98 |
Non-linear solution to the maximum height orbit transfer guidance problem
|
Afshari, H H |
|
2012 |
|
6 |
p. 620-630 |
artikel |
99 |
Non-linear solution to the maximum height orbit transfer guidance problem
|
Afshari, H H |
|
2012 |
|
6 |
p. 620-630 |
artikel |
100 |
Numerical investigation of fragmentation initiation threshold for sphere impacting on thin wall at hypervelocity
|
Zhang, Xiaotian |
|
2016 |
|
6 |
p. 967-980 |
artikel |
101 |
Numerical study on vibration stress of rotating fan blade under aerodynamic load at critical speed
|
Kou, Hai-jun |
|
2016 |
|
6 |
p. 1044-1058 |
artikel |
102 |
Occasion determination method of low Earth orbit satellites meeting the narrow-beam signal
|
Ma, Yiwei |
|
2019 |
|
6 |
p. 2198-2206 |
artikel |
103 |
On-line guidance with trajectory constraints for terminal area energy management of re-entry vehicles
|
Morani, G |
|
2011 |
|
6 |
p. 631-643 |
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 |
|
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 |
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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 |
|
6 |
p. 949-959 |
artikel |
115 |
Results of the GNSS receiver experiment OCAM-G on Ariane-5 flight VA 219
|
Hauschild, André |
|
2017 |
|
6 |
p. 1100-1114 |
artikel |
116 |
Robust adaptive finite time control for spacecraft global attitude tracking maneuvers
|
Gao, Jiwei |
|
2016 |
|
6 |
p. 1027-1043 |
artikel |
117 |
Robust missile longitudinal autopilot design based on equivalent-input-disturbance and generalized extended state observer approach
|
Li, Tong |
|
2015 |
|
6 |
p. 1025-1042 |
artikel |
118 |
Series expansion-based state transition matrix for relative motion on eccentric orbits
|
Li, Yafei |
|
2014 |
|
6 |
p. 869-879 |
artikel |
119 |
Shock environment design for space equipment testing
|
Morais, OMF |
|
2017 |
|
6 |
p. 1154-1167 |
artikel |
120 |
Solid upper stage design process using finite burn maneuvers for low Earth orbit–geosynchronous Earth orbit transfer phase
|
Motlagh, Javad Amiri |
|
2013 |
|
6 |
p. 966-976 |
artikel |
121 |
Spatial trajectory tracking control for unmanned airships based on active disturbance rejection control
|
Lou, Wenjie |
|
2019 |
|
6 |
p. 2231-2240 |
artikel |
122 |
Star selection strategy using measurement coupling matrix in starlight Doppler-based integrated navigation system
|
Liu, Jin |
|
2016 |
|
6 |
p. 1114-1125 |
artikel |
123 |
Structural optimization technique of a T-tail
|
Qiu, Ju |
|
2013 |
|
6 |
p. 1009-1020 |
artikel |
124 |
Synergistic integration of computational fluid dynamics and experimental fluid dynamics for ground effect aerodynamics studies
|
Barber, T J |
|
2012 |
|
6 |
p. 602-619 |
artikel |
125 |
Synergistic integration of computational fluid dynamics and experimental fluid dynamics for ground effect aerodynamics studies
|
Barber, T J |
|
2012 |
|
6 |
p. 602-619 |
artikel |
126 |
The applications of an importance sampling method to reliability analysis of the inside flap of an aircraft
|
Tang, Zhangchun |
|
2013 |
|
6 |
p. 916-932 |
artikel |
127 |
The biojetfuel industry: its rapid emergence, future development, and likely profile
|
Whitfield, R |
|
2011 |
|
6 |
p. 619-630 |
artikel |
128 |
The fault diagnosis of aircraft power system based on inverse problem of fuzzy optimization
|
Cao, Huang |
|
2016 |
|
6 |
p. 1059-1074 |
artikel |
129 |
The study of droplet deformation and droplet volume fraction in an aero-engine bearing chamber
|
Fang, Long |
|
2019 |
|
6 |
p. 2264-2277 |
artikel |
130 |
Three-dimensional united biased proportional navigation law for interception of maneuvering targets with angular constraint
|
Yan, Liang |
|
2015 |
|
6 |
p. 1013-1024 |
artikel |
131 |
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