nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A cubic-spline-based time collocation method applied to simulate periodic transonic flows
|
Du, Pengcheng |
|
2017 |
|
1 |
p. 17-29 |
artikel |
2 |
Adaptive backstepping control for a multi-vectored thrust stratospheric airship with thrust saturation in wind
|
Han, Ding |
|
2016 |
|
1 |
p. 45-59 |
artikel |
3 |
Adaptive nonsingular fast terminal sliding mode control for aircraft with center of gravity variations
|
Han, Chan |
|
2015 |
|
1 |
p. 4-9 |
artikel |
4 |
Adaptive sliding mode backstepping control for entry reusable launch vehicles based on nonlinear disturbance observer
|
Wang, Zhen |
|
2016 |
|
1 |
p. 19-29 |
artikel |
5 |
Adaptive trajectory tracking control system design for hypersonic vehicles with parametric uncertainty
|
Liu, Zhen |
|
2015 |
|
1 |
p. 119-134 |
artikel |
6 |
Aerodynamic design of an ultra-highly loaded booster of a high bypass ratio turbofan
|
Chen, Yuwen |
|
2019 |
|
1 |
p. 240-249 |
artikel |
7 |
Aeroelastic tailoring of composite sandwich panel with lamination parameters
|
Jin, Peng |
|
2016 |
|
1 |
p. 105-117 |
artikel |
8 |
A framework of frequency-domain flight dynamics modeling for multi-rotor aerial vehicles
|
Cai, Guowei |
|
2017 |
|
1 |
p. 30-46 |
artikel |
9 |
A generalized design method for three-dimensional guidance laws
|
Sun, Sheng |
|
2017 |
|
1 |
p. 47-60 |
artikel |
10 |
A Historical Overview on the 25th Anniversary
|
Hodgkinson, John |
|
2014 |
|
1 |
p. 4-6 |
artikel |
11 |
Airflow hazard prediction for helicopter flight in icing condition
|
Cao, Yihua |
|
2014 |
|
1 |
p. 147-154 |
artikel |
12 |
A method for shock train leading edge detection based on differential pressure
|
Xiong, B |
|
2017 |
|
1 |
p. 61-71 |
artikel |
13 |
A modal approach for coupled fluid structure computations of wing flutter
|
Zhong, Jize |
|
2017 |
|
1 |
p. 72-81 |
artikel |
14 |
Analytical and numerical investigations on the penetration of rigid projectiles into the foam core sandwich panels with aluminum face-sheets
|
Alavi Nia, A |
|
2019 |
|
1 |
p. 285-298 |
artikel |
15 |
An analytical investigation of stator lean on rotor–stator interaction noise
|
Liu, Haijian |
|
2015 |
|
1 |
p. 96-109 |
artikel |
16 |
A new direct simulation Monte Carlo implementation for more efficient simulation of hypersonic flow over arbitrarily shaped bodies using dynamic cells
|
Reji, RV |
|
2017 |
|
1 |
p. 82-97 |
artikel |
17 |
A new direct statistical analysis of nonlinear systems: CAUTDET
|
Li, Hong-Xia |
|
2019 |
|
1 |
p. 382-389 |
artikel |
18 |
A new method for online identification of the center of mass of spacecraft using multiple accelerometers
|
He, Huang |
|
2015 |
|
1 |
p. 110-118 |
artikel |
19 |
A novel method for spacecraft electrical fault detection based on FCM clustering and WPSVM classification with PCA feature extraction
|
Li, Ke |
|
2017 |
|
1 |
p. 98-108 |
artikel |
20 |
Anti-unwinding constrained attitude control for flexible spacecraft with actuator saturation
|
Long, Haihui |
|
2016 |
|
1 |
p. 90-104 |
artikel |
21 |
A numerical study on the friction and wear predictions of finger lock chuck in landing gear
|
Zhang, Ming |
|
2017 |
|
1 |
p. 109-123 |
artikel |
22 |
A reliable analytical navigation system based on symmetrical dynamic behavior of control channels
|
Hassani, Mehdi |
|
2017 |
|
1 |
p. 190-199 |
artikel |
23 |
A revision of the flutter margin method to predict in real-time the limit cycle oscillations onset speed with structural freeplay present in the plunge axis
|
Casado Corpas, JL |
|
2017 |
|
1 |
p. 124-142 |
artikel |
24 |
A sampling-based probabilistic path planner for multirotor air vehicles in cluttered environments
|
Brown, Andrew |
|
2017 |
|
1 |
p. 143-162 |
artikel |
25 |
A simple and conservative unstructured sliding-mesh approach for rotor–fuselage aerodynamic interaction simulation
|
Xu, He-Yong |
|
2017 |
|
1 |
p. 163-179 |
artikel |
26 |
A spline wavelet collocation method for the optimal control of flexible spacecraft
|
Zhang, Qingbin |
|
2015 |
|
1 |
p. 163-171 |
artikel |
27 |
A study of a target identification method for an active debris removal system
|
Seong, Jae-Dong |
|
2017 |
|
1 |
p. 180-189 |
artikel |
28 |
Autonomous navigation of spacecraft formation in the proximity of minor bodies
|
Yang, Hui Xin |
|
2016 |
|
1 |
p. 189-204 |
artikel |
29 |
BiGlobal stability analysis of the wake behind an isolated roughness element in hypersonic flow
|
Montero, Iván Padilla |
|
|
|
1 |
p. 5-19 |
artikel |
30 |
Blended wing body lateral-directional stability investigation using 6DOF simulation
|
Roysdon, PF |
|
2014 |
|
1 |
p. 7-19 |
artikel |
31 |
Book Review
|
|
|
1991 |
|
1 |
p. 67 |
artikel |
32 |
Buckling and free vibration analysis of skew sandwich plates with viscoelastic core and functionally graded material constraining layer
|
Joseph, Shince V |
|
2019 |
|
1 |
p. 369-381 |
artikel |
33 |
Calibration for gimbaled platform inertial navigation system on centrifuge
|
Xu, Yong-fei |
|
2019 |
|
1 |
p. 250-260 |
artikel |
34 |
Computational and experimental studies of horizontal tail flutter suppression
|
Khan, Abid Ali |
|
2019 |
|
1 |
p. 34-43 |
artikel |
35 |
Computational study on the hovering mechanisms of a chordwise flexible wing
|
Zhang, X W |
|
2012 |
|
1 |
p. 3-14 |
artikel |
36 |
Computation of global trajectories of commercial transport aircraft
|
Rivas, Damián |
|
2013 |
|
1 |
p. 142-158 |
artikel |
37 |
Contents
|
|
|
1991 |
|
1 |
p. i |
artikel |
38 |
Design and implementation of attitude control algorithm of a satellite on a three-axis gimbal simulator
|
Kabganian, Mansour |
|
2015 |
|
1 |
p. 72-86 |
artikel |
39 |
Design and wind tunnel experimental validation of a controlled new rotary actuation system for a morphing wing application
|
Kammegne, Michel Joël Tchatchueng |
|
2016 |
|
1 |
p. 132-145 |
artikel |
40 |
Design of a robust fault-tolerant control algorithm based on failure mode effects criticality analysis for a three-axis satellite
|
Abedini, Mohammad Reza |
|
2019 |
|
1 |
p. 91-110 |
artikel |
41 |
Design of the wind tunnel based virtual flight testing evaluation method for flight control systems
|
Huang, Min |
|
2018 |
|
1 |
p. 17-29 |
artikel |
42 |
Development of a new method for ATFCM based on trajectory-based operations
|
Gatsinzi, Dany |
|
2019 |
|
1 |
p. 261-284 |
artikel |
43 |
Development of design methodology for a synthetic jet actuator array for flow separation control applications
|
Jabbal, Mark |
|
2013 |
|
1 |
p. 110-124 |
artikel |
44 |
Discussion
|
Heath, W G |
|
1991 |
|
1 |
p. 65 |
artikel |
45 |
Dynamic analysis of finger seal in the complex working state
|
Zhao, Hai-Lin |
|
2019 |
|
1 |
p. 125-137 |
artikel |
46 |
Dynamic modeling and motion precision analysis of spacecraft manipulator with harmonic drive considering the alternate thermal field in orbit
|
Zhao, Jieliang |
|
2015 |
|
1 |
p. 135-148 |
artikel |
47 |
Dynamics and modeling of rocket towed net system
|
Jian, Shen |
|
2018 |
|
1 |
p. 185-197 |
artikel |
48 |
Effective plasma buffet and drag control for laminar transonic aerofoil
|
Polivanov, Pavel A |
|
|
|
1 |
p. 58-67 |
artikel |
49 |
Effect of different triple swirlers on the performance of a triple swirler combustor
|
Ding, Guoyu |
|
2015 |
|
1 |
p. 26-37 |
artikel |
50 |
Effect of finite width cavity in axisymmetric supersonic flow field
|
Jeyakumar, S |
|
2018 |
|
1 |
p. 180-184 |
artikel |
51 |
Effect of inlet distortion on the performance of axial transonic contra-rotating compressor
|
Liu, Hanru |
|
2018 |
|
1 |
p. 42-54 |
artikel |
52 |
Effect of tube lip thickness on the performance of Hartmann–Sprenger tubes
|
Vinoth, B R |
|
2012 |
|
1 |
p. 74-87 |
artikel |
53 |
Effects of inlet radial distortion on the type of stall precursor in low-speed axial compressor
|
Arshad, Ali |
|
2018 |
|
1 |
p. 55-67 |
artikel |
54 |
Effects of periodic wakes on the endwall secondary flow in high-lift low-pressure turbine cascades at low Reynolds numbers
|
Qu, Xiao |
|
2019 |
|
1 |
p. 354-368 |
artikel |
55 |
Effects of space environment temperature on the mechanical properties of carbon fiber/bismaleimide composites laminates
|
Yang, Baifeng |
|
2018 |
|
1 |
p. 3-16 |
artikel |
56 |
Erratum
|
|
|
1991 |
|
1 |
p. 66 |
artikel |
57 |
Evolution of localized artificial disturbance in 2D and 3D supersonic boundary layers
|
Yatskikh, Aleksey |
|
|
|
1 |
p. 115-123 |
artikel |
58 |
Experimental and numerical analyses of gas–solid-multiphase jet in cross-flow
|
Fu, Yao |
|
2013 |
|
1 |
p. 61-79 |
artikel |
59 |
Experimental and numerical helicopter pilot characterization for aeroelastic rotorcraft–pilot coupling analysis
|
Masarati, Pierangelo |
|
2013 |
|
1 |
p. 125-141 |
artikel |
60 |
Experimental study of a small partial admission axial turbine with low aspect ratio blade
|
Varma, AK |
|
2014 |
|
1 |
p. 20-34 |
artikel |
61 |
Feasible footprint generation with uncertainty effects
|
He, Rui-Zhi |
|
2019 |
|
1 |
p. 138-150 |
artikel |
62 |
Finite-time attitude tracking control of air bearing table for spacecraft rendezvous and docking
|
Huang, Cheng |
|
2018 |
|
1 |
p. 96-110 |
artikel |
63 |
Finite-time coordination control for formation flying spacecraft without unwinding
|
Guo, Yong |
|
2016 |
|
1 |
p. 172-188 |
artikel |
64 |
Flutter of a two-dimensional wing with asymmetry at low Mach numbers
|
Shao, Song |
|
2014 |
|
1 |
p. 86-96 |
artikel |
65 |
Force-based delay compensation for hardware-in-the-loop simulation divergence of 6-DOF space contact
|
Wang, Qian |
|
2019 |
|
1 |
p. 151-165 |
artikel |
66 |
Fuel near-optimal guidance law for the powered descending phase of a lunar module
|
Zhang, F |
|
2012 |
|
1 |
p. 108-120 |
artikel |
67 |
Generation of disturbances in the boundary layer of a flat plate by periodic low-frequency motion of the surface section
|
Katasonov, Mikhail M |
|
|
|
1 |
p. 109-114 |
artikel |
68 |
4-GNSS radio occultation satellite constellation design based on Dual-gate uniformity evaluation index
|
Wang, Jue-yao |
|
2017 |
|
1 |
p. 3-16 |
artikel |
69 |
Guidelines for Authors
|
|
|
1991 |
|
1 |
p. ii |
artikel |
70 |
Improvement of satellite conflict prediction reliability through use of the adaptive splitting technique
|
Pastel, Rudy |
|
2014 |
|
1 |
p. 77-85 |
artikel |
71 |
Improving the UAS-S4 Éhecal airfoil high angles-of-attack performance characteristics using a morphing wing approach
|
Gabor, Oliviu Şugar |
|
2016 |
|
1 |
p. 118-131 |
artikel |
72 |
Improving two axes gimbal seeker performance using cascade control approach
|
Abdo, Maher Mahmoud |
|
2015 |
|
1 |
p. 38-55 |
artikel |
73 |
Influence of clamp band joint on dynamic behavior of launching system in ascent flight
|
Qin, ZY |
|
2014 |
|
1 |
p. 97-114 |
artikel |
74 |
Influence of two-dimensional roughness element on boundary layer structure in the favourable pressure gradient region of the swept wing
|
Tolkachev, Stepan |
|
|
|
1 |
p. 20-27 |
artikel |
75 |
In memoriam of Sergio Chiesa, revered Aerospace Engineering Professor by Rodrigo Martinez-Val
|
|
|
2015 |
|
1 |
p. 3-3 |
artikel |
76 |
Integrated flight/propulsion optimal control for DPC aircraft based on the GA-RPS algorithm
|
Zhang, Jing |
|
2016 |
|
1 |
p. 157-171 |
artikel |
77 |
Integrated motion planning and trajectory control system for unmanned air vehicles
|
Karimi, J |
|
2013 |
|
1 |
p. 3-18 |
artikel |
78 |
Integrated system health management-based condition assessment for manned spacecraft avionics
|
Xu, Jiuping |
|
2013 |
|
1 |
p. 19-32 |
artikel |
79 |
Integrated versus two-loop guidance-autopilot for a dual control missile with high-order aerodynamic model
|
Ibarrondo, FB |
|
2016 |
|
1 |
p. 60-76 |
artikel |
80 |
Intelligent attitude planning algorithm based on the characteristics of low radar cross section characteristics of microsatellites under complex constraints
|
Hua, Bing |
|
2019 |
|
1 |
p. 4-21 |
artikel |
81 |
Introduction to Special Issue on boundary layer transition
|
Knight, Doyle D |
|
|
|
1 |
p. 3-4 |
artikel |
82 |
Investigation on a multispar composite wing
|
Stamatelos, D G |
|
2012 |
|
1 |
p. 88-96 |
artikel |
83 |
Laminar buffet and flow control
|
Brion, V |
|
|
|
1 |
p. 124-139 |
artikel |
84 |
Laminar–turbulent transition reversal on blunt ogive body of revolution at hypersonic speeds
|
Vaganov, A |
|
|
|
1 |
p. 102-108 |
artikel |
85 |
Landing Gear—the Aircraft Requirement
|
Greenbank, S J |
|
1991 |
|
1 |
p. 27-34 |
artikel |
86 |
Laser Anemometry in Turbomachines
|
Ahmed, N A |
|
1991 |
|
1 |
p. 1-12 |
artikel |
87 |
Linear covariance techniques for closed-loop guidance navigation and control system design and analysis
|
Christensen, Randall S |
|
2014 |
|
1 |
p. 44-65 |
artikel |
88 |
Line-of-sight stabilization of a gimbaled mechanism under passive base isolation
|
Kandemir, Kutlu Demir |
|
2014 |
|
1 |
p. 35-43 |
artikel |
89 |
Localized micro-discharges group dielectric barrier discharge vortex generators: Disturbances source for active transition control
|
Moralev, Ivan |
|
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|
1 |
p. 42-57 |
artikel |
90 |
Locally-optimal electric sail transfer
|
Bassetto, Marco |
|
2019 |
|
1 |
p. 166-179 |
artikel |
91 |
Main helicopter rotor trimming using computational fluid dynamics method in forward flight
|
Ma, Yimin |
|
2018 |
|
1 |
p. 169-179 |
artikel |
92 |
Mathematical modelling, simulation, and estimation of aircraft parameters using five degree-of-freedom dynamic test rig
|
Peyada, N K |
|
2012 |
|
1 |
p. 55-63 |
artikel |
93 |
Modified federated Kalman filter for INS/GNSS/CNS integration
|
Hu, Gaoge |
|
2016 |
|
1 |
p. 30-44 |
artikel |
94 |
Multidisciplinary mission design optimization for space launch vehicles based on sequential design process
|
Shu, Jung-Il |
|
2016 |
|
1 |
p. 3-18 |
artikel |
95 |
Non-cooperative maritime target position and velocity measuring method based on monocular trajectory intersection for video satellite
|
Chen, Shengyi |
|
2019 |
|
1 |
p. 44-56 |
artikel |
96 |
Nonlinear dynamic characteristics of rotating ramjet rotor supported by hybrid gas bearing
|
Zhang, Guang-hui |
|
2014 |
|
1 |
p. 115-136 |
artikel |
97 |
Non-linear flight control for unmanned aerial vehicles using adaptive backstepping based on invariant manifolds
|
Zhang, Jiaming |
|
2013 |
|
1 |
p. 33-44 |
artikel |
98 |
Nonlinear L1 adaptive control of an airplane with structural damage
|
Ahmadi, Karim |
|
2019 |
|
1 |
p. 341-353 |
artikel |
99 |
Nonlinear static analysis-based thrust for solar sail
|
Liu, Jiafu |
|
2015 |
|
1 |
p. 149-162 |
artikel |
100 |
Novel probabilistic dynamic safety metric formulations for flight path determination
|
Sarigul-Klijn, Nesrin |
|
2013 |
|
1 |
p. 185-198 |
artikel |
101 |
Numerical and experimental investigations on flow regulation of fuel vapor core pump
|
Wang, Bin |
|
2018 |
|
1 |
p. 111-120 |
artikel |
102 |
Numerical investigation of boundary layer suction on certain highly loaded aspirated compressor at low speeds
|
Chen, Shaowen |
|
2018 |
|
1 |
p. 30-41 |
artikel |
103 |
Numerical investigation of flexible flapping wings using computational fluid dynamics/computational structural dynamics method
|
Liu, Long |
|
2018 |
|
1 |
p. 85-95 |
artikel |
104 |
Numerical prediction of unsteady aerodynamics for a ducted fan micro air vehicle
|
Cai, Hongming |
|
2015 |
|
1 |
p. 87-95 |
artikel |
105 |
Numerical simulation of jet mixing enhancement using rectangular control jets
|
Eri, Qitai |
|
2019 |
|
1 |
p. 111-124 |
artikel |
106 |
Numerical study of wall cooling effects on transition between shock structures in a rocket propulsion nozzle
|
Kharati-Koopaee, Masoud |
|
2015 |
|
1 |
p. 172-184 |
artikel |
107 |
Optimal attitude trajectory planning method for CMG actuated spacecraft
|
Zhang, Lijun |
|
2018 |
|
1 |
p. 131-142 |
artikel |
108 |
Optimal linear attitude estimator and its recursive algorithm via geometric analysis
|
Gong, Deren |
|
2013 |
|
1 |
p. 100-109 |
artikel |
109 |
Optimization of space radiators accounting for variable thermal conductivity and base-to-fin radiation interaction
|
Arslanturk, Cihat |
|
2018 |
|
1 |
p. 121-130 |
artikel |
110 |
Optimizing multidisciplinary scaled tests in terrestrial atmosphere for extraterrestrial unmanned aerial vehicle missions
|
Moreno, Ana I |
|
2016 |
|
1 |
p. 77-89 |
artikel |
111 |
Parabolized stability analysis of chemically reacting boundary-layer flows in equilibrium conditions
|
Zanus, Ludovico |
|
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1 |
p. 79-95 |
artikel |
112 |
Particle image velocimetry study of the impinging height effect on an overexpanded supersonic impinging free jet at Ma = 1.754. Part 1: global coherent structure
|
Xu, J L |
|
2012 |
|
1 |
p. 64-73 |
artikel |
113 |
Path-following control for fixed-wing unmanned aerial vehicles based on a virtual target
|
Zhang, JM |
|
2014 |
|
1 |
p. 66-76 |
artikel |
114 |
Performance analysis of a federated ultra-tight global positioning system/inertial navigation system integration algorithm in high dynamic environments
|
Xie, Fei |
|
2015 |
|
1 |
p. 56-71 |
artikel |
115 |
Performance analysis of BDS for regional services with consideration on weighted factors
|
Zhang, Pengfei |
|
2016 |
|
1 |
p. 146-156 |
artikel |
116 |
Performance study of an inlet in supersonic flow
|
Soltani, Mohammad R |
|
2013 |
|
1 |
p. 159-174 |
artikel |
117 |
Persistent surveillance for a swarm of micro aerial vehicles by flocking algorithm
|
Li, Wei |
|
2015 |
|
1 |
p. 185-194 |
artikel |
118 |
Prediction of boundary layer transition on a flat plate subject to surface waviness
|
Lin, Y |
|
2012 |
|
1 |
p. 42-54 |
artikel |
119 |
Pressure gradient effects on wake-flow instabilities behind isolated roughness elements on re-entry capsules
|
Theiss, Alexander |
|
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1 |
p. 28-41 |
artikel |
120 |
Propulsion Systems for Twenty-First Century Commercial Transports
|
Powell, D T |
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1991 |
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1 |
p. 13-26 |
artikel |
121 |
Quality and reliability in engineering
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Place, S |
|
2013 |
|
1 |
p. 209-209 |
artikel |
122 |
Quality Costing at British Aerospace Dynamics: A Case Study
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Hesford, M G |
|
1991 |
|
1 |
p. 53-57 |
artikel |
123 |
Rate regulation of a suborbital reentry payload by moving-mass actuators
|
Mohammadi, Aidin |
|
2013 |
|
1 |
p. 80-92 |
artikel |
124 |
Residual life prediction from statistical features and a GARCH modeling approach for aircraft generators
|
Du, Xiaofei |
|
2014 |
|
1 |
p. 137-146 |
artikel |
125 |
Response of an oblique shock train to downstream periodic pressure perturbations
|
Cheng, Chuan |
|
2019 |
|
1 |
p. 57-70 |
artikel |
126 |
Rigid–flexible coupled dynamics analysis for solar sails
|
Liu, Jiafu |
|
2019 |
|
1 |
p. 324-340 |
artikel |
127 |
Robust adaptive attitude tracking coordination control for spacecraft formation with unknown time-varying inertia
|
Zhu, Zhihao |
|
2019 |
|
1 |
p. 310-323 |
artikel |
128 |
Robust adaptive backstepping tracking control for a flexible air-breathing hypersonic vehicle subject to input constraint
|
Zong, Q |
|
2015 |
|
1 |
p. 10-25 |
artikel |
129 |
Robust autopilot design of uncertain bank-to-turn missiles using state-space disturbance observers
|
Yang, J |
|
2012 |
|
1 |
p. 97-107 |
artikel |
130 |
Robust-extended Kalman filter for small satellite attitude estimation in the presence of measurement uncertainties and faults
|
Xing, Y |
|
2012 |
|
1 |
p. 30-41 |
artikel |
131 |
Rotor-state feedback control design to improve helicopter turbulence alleviation in hover
|
Ji, Honglei |
|
2018 |
|
1 |
p. 156-168 |
artikel |
132 |
Satellite constellation build-up via three-body dynamics
|
Nadoushan, Mahdi Jafari |
|
2014 |
|
1 |
p. 155-160 |
artikel |
133 |
Sensor faults tolerance control for a novel multi-rotor aircraft based on sliding mode control
|
Fu, Chunyang |
|
2019 |
|
1 |
p. 180-196 |
artikel |
134 |
Shape pre-adjustment of deployable mesh antennas considering space thermal loads
|
Yang, Guigeng |
|
2018 |
|
1 |
p. 143-155 |
artikel |
135 |
Simple surrogate models to determine total accessibility duration of low Earth orbit sunsynchronous satellites
|
Khamseh, Hossein Bonyan |
|
2013 |
|
1 |
p. 45-60 |
artikel |
136 |
Simultaneous attack strategy against a maneuvering target with unknown acceleration
|
Hu, Zilun |
|
2019 |
|
1 |
p. 71-80 |
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