| no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
| 1 |
A cubic-spline-based time collocation method applied to simulate periodic transonic flows
|
Du, Pengcheng
|
|
2017
|
|
1 |
p. 17-29
|
article
|
| 2 |
Adaptive backstepping control for a multi-vectored thrust stratospheric airship with thrust saturation in wind
|
Han, Ding
|
|
2016
|
|
1 |
p. 45-59
|
article
|
| 3 |
Adaptive nonsingular fast terminal sliding mode control for aircraft with center of gravity variations
|
Han, Chan
|
|
2015
|
|
1 |
p. 4-9
|
article
|
| 4 |
Adaptive sliding mode backstepping control for entry reusable launch vehicles based on nonlinear disturbance observer
|
Wang, Zhen
|
|
2016
|
|
1 |
p. 19-29
|
article
|
| 5 |
Adaptive trajectory tracking control system design for hypersonic vehicles with parametric uncertainty
|
Liu, Zhen
|
|
2015
|
|
1 |
p. 119-134
|
article
|
| 6 |
Aerodynamic design of an ultra-highly loaded booster of a high bypass ratio turbofan
|
Chen, Yuwen
|
|
2019
|
|
1 |
p. 240-249
|
article
|
| 7 |
Aeroelastic tailoring of composite sandwich panel with lamination parameters
|
Jin, Peng
|
|
2016
|
|
1 |
p. 105-117
|
article
|
| 8 |
A framework of frequency-domain flight dynamics modeling for multi-rotor aerial vehicles
|
Cai, Guowei
|
|
2017
|
|
1 |
p. 30-46
|
article
|
| 9 |
A generalized design method for three-dimensional guidance laws
|
Sun, Sheng
|
|
2017
|
|
1 |
p. 47-60
|
article
|
| 10 |
A Historical Overview on the 25th Anniversary
|
Hodgkinson, John
|
|
2014
|
|
1 |
p. 4-6
|
article
|
| 11 |
Airflow hazard prediction for helicopter flight in icing condition
|
Cao, Yihua
|
|
2014
|
|
1 |
p. 147-154
|
article
|
| 12 |
A method for shock train leading edge detection based on differential pressure
|
Xiong, B
|
|
2017
|
|
1 |
p. 61-71
|
article
|
| 13 |
A modal approach for coupled fluid structure computations of wing flutter
|
Zhong, Jize
|
|
2017
|
|
1 |
p. 72-81
|
article
|
| 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
|
article
|
| 15 |
An analytical investigation of stator lean on rotor–stator interaction noise
|
Liu, Haijian
|
|
2015
|
|
1 |
p. 96-109
|
article
|
| 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
|
article
|
| 17 |
A new direct statistical analysis of nonlinear systems: CAUTDET
|
Li, Hong-Xia
|
|
2019
|
|
1 |
p. 382-389
|
article
|
| 18 |
A new method for online identification of the center of mass of spacecraft using multiple accelerometers
|
He, Huang
|
|
2015
|
|
1 |
p. 110-118
|
article
|
| 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
|
article
|
| 20 |
Anti-unwinding constrained attitude control for flexible spacecraft with actuator saturation
|
Long, Haihui
|
|
2016
|
|
1 |
p. 90-104
|
article
|
| 21 |
A numerical study on the friction and wear predictions of finger lock chuck in landing gear
|
Zhang, Ming
|
|
2017
|
|
1 |
p. 109-123
|
article
|
| 22 |
A reliable analytical navigation system based on symmetrical dynamic behavior of control channels
|
Hassani, Mehdi
|
|
2017
|
|
1 |
p. 190-199
|
article
|
| 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
|
article
|
| 24 |
A sampling-based probabilistic path planner for multirotor air vehicles in cluttered environments
|
Brown, Andrew
|
|
2017
|
|
1 |
p. 143-162
|
article
|
| 25 |
A simple and conservative unstructured sliding-mesh approach for rotor–fuselage aerodynamic interaction simulation
|
Xu, He-Yong
|
|
2017
|
|
1 |
p. 163-179
|
article
|
| 26 |
A spline wavelet collocation method for the optimal control of flexible spacecraft
|
Zhang, Qingbin
|
|
2015
|
|
1 |
p. 163-171
|
article
|
| 27 |
A study of a target identification method for an active debris removal system
|
Seong, Jae-Dong
|
|
2017
|
|
1 |
p. 180-189
|
article
|
| 28 |
Autonomous navigation of spacecraft formation in the proximity of minor bodies
|
Yang, Hui Xin
|
|
2016
|
|
1 |
p. 189-204
|
article
|
| 29 |
BiGlobal stability analysis of the wake behind an isolated roughness element in hypersonic flow
|
Montero, Iván Padilla
|
|
|
|
1 |
p. 5-19
|
article
|
| 30 |
Blended wing body lateral-directional stability investigation using 6DOF simulation
|
Roysdon, PF
|
|
2014
|
|
1 |
p. 7-19
|
article
|
| 31 |
Book Review
|
|
|
1991
|
|
1 |
p. 67
|
article
|
| 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
|
article
|
| 33 |
Calibration for gimbaled platform inertial navigation system on centrifuge
|
Xu, Yong-fei
|
|
2019
|
|
1 |
p. 250-260
|
article
|
| 34 |
Computational and experimental studies of horizontal tail flutter suppression
|
Khan, Abid Ali
|
|
2019
|
|
1 |
p. 34-43
|
article
|
| 35 |
Computational study on the hovering mechanisms of a chordwise flexible wing
|
Zhang, X W
|
|
2012
|
|
1 |
p. 3-14
|
article
|
| 36 |
Computation of global trajectories of commercial transport aircraft
|
Rivas, Damián
|
|
2013
|
|
1 |
p. 142-158
|
article
|
| 37 |
Contents
|
|
|
1991
|
|
1 |
p. i
|
article
|
| 38 |
Design and implementation of attitude control algorithm of a satellite on a three-axis gimbal simulator
|
Kabganian, Mansour
|
|
2015
|
|
1 |
p. 72-86
|
article
|
| 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
|
article
|
| 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
|
article
|
| 41 |
Design of the wind tunnel based virtual flight testing evaluation method for flight control systems
|
Huang, Min
|
|
2018
|
|
1 |
p. 17-29
|
article
|
| 42 |
Development of a new method for ATFCM based on trajectory-based operations
|
Gatsinzi, Dany
|
|
2019
|
|
1 |
p. 261-284
|
article
|
| 43 |
Development of design methodology for a synthetic jet actuator array for flow separation control applications
|
Jabbal, Mark
|
|
2013
|
|
1 |
p. 110-124
|
article
|
| 44 |
Discussion
|
Heath, W G
|
|
1991
|
|
1 |
p. 65
|
article
|
| 45 |
Dynamic analysis of finger seal in the complex working state
|
Zhao, Hai-Lin
|
|
2019
|
|
1 |
p. 125-137
|
article
|
| 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
|
article
|
| 47 |
Dynamics and modeling of rocket towed net system
|
Jian, Shen
|
|
2018
|
|
1 |
p. 185-197
|
article
|
| 48 |
Effective plasma buffet and drag control for laminar transonic aerofoil
|
Polivanov, Pavel A
|
|
|
|
1 |
p. 58-67
|
article
|
| 49 |
Effect of different triple swirlers on the performance of a triple swirler combustor
|
Ding, Guoyu
|
|
2015
|
|
1 |
p. 26-37
|
article
|
| 50 |
Effect of finite width cavity in axisymmetric supersonic flow field
|
Jeyakumar, S
|
|
2018
|
|
1 |
p. 180-184
|
article
|
| 51 |
Effect of inlet distortion on the performance of axial transonic contra-rotating compressor
|
Liu, Hanru
|
|
2018
|
|
1 |
p. 42-54
|
article
|
| 52 |
Effect of tube lip thickness on the performance of Hartmann–Sprenger tubes
|
Vinoth, B R
|
|
2012
|
|
1 |
p. 74-87
|
article
|
| 53 |
Effects of inlet radial distortion on the type of stall precursor in low-speed axial compressor
|
Arshad, Ali
|
|
2018
|
|
1 |
p. 55-67
|
article
|
| 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
|
article
|
| 55 |
Effects of space environment temperature on the mechanical properties of carbon fiber/bismaleimide composites laminates
|
Yang, Baifeng
|
|
2018
|
|
1 |
p. 3-16
|
article
|
| 56 |
Erratum
|
|
|
1991
|
|
1 |
p. 66
|
article
|
| 57 |
Evolution of localized artificial disturbance in 2D and 3D supersonic boundary layers
|
Yatskikh, Aleksey
|
|
|
|
1 |
p. 115-123
|
article
|
| 58 |
Experimental and numerical analyses of gas–solid-multiphase jet in cross-flow
|
Fu, Yao
|
|
2013
|
|
1 |
p. 61-79
|
article
|
| 59 |
Experimental and numerical helicopter pilot characterization for aeroelastic rotorcraft–pilot coupling analysis
|
Masarati, Pierangelo
|
|
2013
|
|
1 |
p. 125-141
|
article
|
| 60 |
Experimental study of a small partial admission axial turbine with low aspect ratio blade
|
Varma, AK
|
|
2014
|
|
1 |
p. 20-34
|
article
|
| 61 |
Feasible footprint generation with uncertainty effects
|
He, Rui-Zhi
|
|
2019
|
|
1 |
p. 138-150
|
article
|
| 62 |
Finite-time attitude tracking control of air bearing table for spacecraft rendezvous and docking
|
Huang, Cheng
|
|
2018
|
|
1 |
p. 96-110
|
article
|
| 63 |
Finite-time coordination control for formation flying spacecraft without unwinding
|
Guo, Yong
|
|
2016
|
|
1 |
p. 172-188
|
article
|
| 64 |
Flutter of a two-dimensional wing with asymmetry at low Mach numbers
|
Shao, Song
|
|
2014
|
|
1 |
p. 86-96
|
article
|
| 65 |
Force-based delay compensation for hardware-in-the-loop simulation divergence of 6-DOF space contact
|
Wang, Qian
|
|
2019
|
|
1 |
p. 151-165
|
article
|
| 66 |
Fuel near-optimal guidance law for the powered descending phase of a lunar module
|
Zhang, F
|
|
2012
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1 |
p. 108-120
|
article
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| 67 |
Generation of disturbances in the boundary layer of a flat plate by periodic low-frequency motion of the surface section
|
Katasonov, Mikhail M
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1 |
p. 109-114
|
article
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| 68 |
4-GNSS radio occultation satellite constellation design based on Dual-gate uniformity evaluation index
|
Wang, Jue-yao
|
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2017
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1 |
p. 3-16
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article
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| 69 |
Guidelines for Authors
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1991
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1 |
p. ii
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article
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| 70 |
Improvement of satellite conflict prediction reliability through use of the adaptive splitting technique
|
Pastel, Rudy
|
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2014
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1 |
p. 77-85
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article
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| 71 |
Improving the UAS-S4 Éhecal airfoil high angles-of-attack performance characteristics using a morphing wing approach
|
Gabor, Oliviu Şugar
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2016
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1 |
p. 118-131
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article
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| 72 |
Improving two axes gimbal seeker performance using cascade control approach
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Abdo, Maher Mahmoud
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2015
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1 |
p. 38-55
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article
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| 73 |
Influence of clamp band joint on dynamic behavior of launching system in ascent flight
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Qin, ZY
|
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2014
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1 |
p. 97-114
|
article
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| 74 |
Influence of two-dimensional roughness element on boundary layer structure in the favourable pressure gradient region of the swept wing
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Tolkachev, Stepan
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1 |
p. 20-27
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article
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| 75 |
In memoriam of Sergio Chiesa, revered Aerospace Engineering Professor by Rodrigo Martinez-Val
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2015
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1 |
p. 3-3
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article
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| 76 |
Integrated flight/propulsion optimal control for DPC aircraft based on the GA-RPS algorithm
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Zhang, Jing
|
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2016
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1 |
p. 157-171
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article
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| 77 |
Integrated motion planning and trajectory control system for unmanned air vehicles
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Karimi, J
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2013
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p. 3-18
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article
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| 78 |
Integrated system health management-based condition assessment for manned spacecraft avionics
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Xu, Jiuping
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2013
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p. 19-32
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article
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| 79 |
Integrated versus two-loop guidance-autopilot for a dual control missile with high-order aerodynamic model
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Ibarrondo, FB
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2016
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p. 60-76
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article
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| 80 |
Intelligent attitude planning algorithm based on the characteristics of low radar cross section characteristics of microsatellites under complex constraints
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Hua, Bing
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2019
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p. 4-21
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article
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| 81 |
Introduction to Special Issue on boundary layer transition
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Knight, Doyle D
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1 |
p. 3-4
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article
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| 82 |
Investigation on a multispar composite wing
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Stamatelos, D G
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2012
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p. 88-96
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article
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| 83 |
Laminar buffet and flow control
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Brion, V
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p. 124-139
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article
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| 84 |
Laminar–turbulent transition reversal on blunt ogive body of revolution at hypersonic speeds
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Vaganov, A
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p. 102-108
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article
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| 85 |
Landing Gear—the Aircraft Requirement
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Greenbank, S J
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p. 27-34
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| 86 |
Laser Anemometry in Turbomachines
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Ahmed, N A
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Linear covariance techniques for closed-loop guidance navigation and control system design and analysis
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Christensen, Randall S
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Line-of-sight stabilization of a gimbaled mechanism under passive base isolation
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Kandemir, Kutlu Demir
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2014
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p. 35-43
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| 89 |
Localized micro-discharges group dielectric barrier discharge vortex generators: Disturbances source for active transition control
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Moralev, Ivan
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p. 42-57
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Locally-optimal electric sail transfer
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Bassetto, Marco
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2019
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p. 166-179
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| 91 |
Main helicopter rotor trimming using computational fluid dynamics method in forward flight
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Ma, Yimin
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Mathematical modelling, simulation, and estimation of aircraft parameters using five degree-of-freedom dynamic test rig
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Peyada, N K
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Modified federated Kalman filter for INS/GNSS/CNS integration
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Hu, Gaoge
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Multidisciplinary mission design optimization for space launch vehicles based on sequential design process
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Shu, Jung-Il
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Non-cooperative maritime target position and velocity measuring method based on monocular trajectory intersection for video satellite
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Chen, Shengyi
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2019
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Nonlinear dynamic characteristics of rotating ramjet rotor supported by hybrid gas bearing
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Zhang, Guang-hui
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Non-linear flight control for unmanned aerial vehicles using adaptive backstepping based on invariant manifolds
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Nonlinear L1 adaptive control of an airplane with structural damage
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Nonlinear static analysis-based thrust for solar sail
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Novel probabilistic dynamic safety metric formulations for flight path determination
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Numerical and experimental investigations on flow regulation of fuel vapor core pump
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Wang, Bin
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2018
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p. 111-120
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| 102 |
Numerical investigation of boundary layer suction on certain highly loaded aspirated compressor at low speeds
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Numerical investigation of flexible flapping wings using computational fluid dynamics/computational structural dynamics method
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Numerical prediction of unsteady aerodynamics for a ducted fan micro air vehicle
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Numerical simulation of jet mixing enhancement using rectangular control jets
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Numerical study of wall cooling effects on transition between shock structures in a rocket propulsion nozzle
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Optimal attitude trajectory planning method for CMG actuated spacecraft
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Optimal linear attitude estimator and its recursive algorithm via geometric analysis
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Optimization of space radiators accounting for variable thermal conductivity and base-to-fin radiation interaction
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Optimizing multidisciplinary scaled tests in terrestrial atmosphere for extraterrestrial unmanned aerial vehicle missions
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Parabolized stability analysis of chemically reacting boundary-layer flows in equilibrium conditions
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Zanus, Ludovico
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p. 79-95
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article
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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
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Xu, J L
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2012
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p. 64-73
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Path-following control for fixed-wing unmanned aerial vehicles based on a virtual target
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Zhang, JM
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Performance analysis of a federated ultra-tight global positioning system/inertial navigation system integration algorithm in high dynamic environments
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2015
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Performance analysis of BDS for regional services with consideration on weighted factors
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2016
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p. 146-156
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Performance study of an inlet in supersonic flow
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Soltani, Mohammad R
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2013
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p. 159-174
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Persistent surveillance for a swarm of micro aerial vehicles by flocking algorithm
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2015
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p. 185-194
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Prediction of boundary layer transition on a flat plate subject to surface waviness
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Lin, Y
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2012
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article
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Pressure gradient effects on wake-flow instabilities behind isolated roughness elements on re-entry capsules
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Theiss, Alexander
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article
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| 120 |
Propulsion Systems for Twenty-First Century Commercial Transports
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Powell, D T
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article
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Quality and reliability in engineering
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