| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A case study involving continuous system methods of inverse simulation for an unmanned aerial vehicle application
|
Murray-Smith, DJ
|
|
2015
|
|
14 |
p. 2700-2717
|
artikel
|
| 2 |
A comparison of accelerometer and piezofilm-based force balances for hypersonic shock tunnels
|
Nanda, Soumya Ranjan
|
|
2019
|
|
14 |
p. 5310-5320
|
artikel
|
| 3 |
Adaptive estimation algorithm of boost-phase trajectory using binary asynchronous observation
|
Wu, Nan
|
|
2016
|
|
14 |
p. 2661-2672
|
artikel
|
| 4 |
Aerodynamics of aero-engine installation
|
Stańkowski, Tomasz P
|
|
2016
|
|
14 |
p. 2673-2692
|
artikel
|
| 5 |
Altitude consensus based 3D flocking control for fixed-wing unmanned aerial vehicle swarm trajectory tracking
|
Zhang, Xiangyin
|
|
2016
|
|
14 |
p. 2628-2638
|
artikel
|
| 6 |
A mixed-fidelity computational model of aero engine for inlet distortion
|
Guo, Jin
|
|
2019
|
|
14 |
p. 5295-5309
|
artikel
|
| 7 |
Amphibious airplane for underwater observation: Conceptual design
|
Yoshida, Yuki
|
|
2018
|
|
14 |
p. 2627-2637
|
artikel
|
| 8 |
An advanced algorithm for recognizing wind shear using airborne Doppler weather radar
|
Wang, Lei
|
|
2015
|
|
14 |
p. 2547-2558
|
artikel
|
| 9 |
An energy method for flutter analysis of wing using one-way fluid structure coupling
|
Zhong, Jize
|
|
2017
|
|
14 |
p. 2560-2569
|
artikel
|
| 10 |
An integrated algorithm for hypersonic fluid–thermal–structural analysis of aerodynamically heated cylindrical leading edge
|
Li, Jiawei
|
|
2019
|
|
14 |
p. 5177-5191
|
artikel
|
| 11 |
A novel satellite cluster design based on tree architecture
|
He, Huang
|
|
2015
|
|
14 |
p. 2659-2670
|
artikel
|
| 12 |
A research on the compressor blade tip pressure modeling and stall detection measure
|
Sun, Fengyong
|
|
2016
|
|
14 |
p. 2654-2660
|
artikel
|
| 13 |
Asymmetric ground effects of a tailless unmanned aerial vehicle model
|
Yang, Muqing
|
|
2014
|
|
14 |
p. 2652-2661
|
artikel
|
| 14 |
Asymmetric ground effects of a tailless unmanned aerial vehicle model
|
Yang, Muqing
|
|
2014
|
|
14 |
p. 2652-2661
|
artikel
|
| 15 |
Attitude determination using Newton’s method on Riemannian manifold
|
Yang, Yaguang
|
|
2015
|
|
14 |
p. 2737-2742
|
artikel
|
| 16 |
Automatic landing control using H-inf control and dynamic inversion
|
Lungu, Romulus
|
|
2014
|
|
14 |
p. 2612-2626
|
artikel
|
| 17 |
Automatic landing control using H-inf control and dynamic inversion
|
Lungu, Romulus
|
|
2014
|
|
14 |
p. 2612-2626
|
artikel
|
| 18 |
Autonomous celestial navigation for a deep space probe approaching a target planet based on ephemeris correction
|
Ma, Xin
|
|
2015
|
|
14 |
p. 2681-2699
|
artikel
|
| 19 |
Autonomous waypoint guidance for tilt-rotor unmanned aerial vehicle that has nacelle-fixed auxiliary wings
|
Kang, Youngshin
|
|
2014
|
|
14 |
p. 2695-2717
|
artikel
|
| 20 |
Autonomous waypoint guidance for tilt-rotor unmanned aerial vehicle that has nacelle-fixed auxiliary wings
|
Kang, Youngshin
|
|
2014
|
|
14 |
p. 2695-2717
|
artikel
|
| 21 |
Combined active flow and flight control systems design for morphing unmanned aerial vehicles
|
Kanat, Öztürk Özdemir
|
|
2019
|
|
14 |
p. 5393-5402
|
artikel
|
| 22 |
Comparison between novel waverider generated from flow past a pointed von Karman ogive and conventional cone-derived waverider
|
Ding, Feng
|
|
2015
|
|
14 |
p. 2620-2633
|
artikel
|
| 23 |
Conceptual design methodology of a box wing aircraft: A novel commercial airliner
|
Kaparos, Pavlos
|
|
2018
|
|
14 |
p. 2651-2662
|
artikel
|
| 24 |
Conceptual design study of a geared turbofan and an open rotor aero engine with intercooled recuperated core
|
Salpingidou, C
|
|
2018
|
|
14 |
p. 2713-2720
|
artikel
|
| 25 |
Conceptual study of a mechanically integrated parallel hybrid electric turbofan
|
Seitz, Arne
|
|
2018
|
|
14 |
p. 2688-2712
|
artikel
|
| 26 |
Design and analysis of a cooling system for a supersonic exhaust diffuser
|
Farahani, M
|
|
2019
|
|
14 |
p. 5253-5263
|
artikel
|
| 27 |
Design and testing of three tailless unmanned aerial vehicle configurations built for surveillance in Antarctic environment
|
Rodzewicz, Miroslaw
|
|
2018
|
|
14 |
p. 2598-2614
|
artikel
|
| 28 |
Design of morphing wing with surface discontinuity
|
Tarnowski, Andrzej
|
|
2018
|
|
14 |
p. 2638-2650
|
artikel
|
| 29 |
Development of rational hybrid fuselage structure for prospective civil aircraft
|
Dubovikov, E
|
|
2018
|
|
14 |
p. 2673-2680
|
artikel
|
| 30 |
Disturbance analysis and feed-forward compensation for the flexible solar array sun-tracking drive
|
Zhu, Shiyao
|
|
2015
|
|
14 |
p. 2646-2658
|
artikel
|
| 31 |
Dynamics design for multiple launch rocket system using transfer matrix method for multibody system
|
Tang, Wenbing
|
|
2016
|
|
14 |
p. 2557-2568
|
artikel
|
| 32 |
Editorial
|
Goraj, Zdobyslaw
|
|
2018
|
|
14 |
p. 2595-2597
|
artikel
|
| 33 |
Effect of axial skewed slot casing treatment in a transonic fan
|
Khaleghi, Hossein
|
|
2017
|
|
14 |
p. 2646-2653
|
artikel
|
| 34 |
Effect of circumferential static pressure nonuniformity caused by volute on tip leakage flow in a centrifugal compressor
|
Fu, Li
|
|
2019
|
|
14 |
p. 5134-5149
|
artikel
|
| 35 |
Effects of aeroelasticity on coning motion of a spinning missile
|
Shi, Zhongjiao
|
|
2016
|
|
14 |
p. 2581-2595
|
artikel
|
| 36 |
Effects of anisotropic composite skin on electrothermal anti-icing system
|
Shen, Xiaobin
|
|
2019
|
|
14 |
p. 5403-5413
|
artikel
|
| 37 |
Experience with the design of ultralight airplane with unconventional powerplant
|
Theiner, R
|
|
2018
|
|
14 |
p. 2721-2733
|
artikel
|
| 38 |
Experimental analysis of shock stand-off distance over spherical bodies in high-enthalpy flows
|
Thakur, Ruchi
|
|
2017
|
|
14 |
p. 2666-2676
|
artikel
|
| 39 |
Experimental investigation on flow unsteadiness during spike stall suppression process in an axial compressor via air injection
|
Taghavi Zenouz, R
|
|
2017
|
|
14 |
p. 2677-2688
|
artikel
|
| 40 |
Experimental investigation on forced response of mistuned bladed disc rotor in an aero-engine
|
Madhavan, S
|
|
2015
|
|
14 |
p. 2572-2588
|
artikel
|
| 41 |
Experimental study on the characteristics of axisymmetric cavity actuated supersonic flow
|
Jeyakumar, S
|
|
2017
|
|
14 |
p. 2570-2577
|
artikel
|
| 42 |
Extended harmonic disturbance observer-based attitude control for flexible spacecraft with control moment gyroscopes
|
Huang, Liya
|
|
2019
|
|
14 |
p. 5331-5346
|
artikel
|
| 43 |
Extended state observer based impact angle constrained guidance law for maneuvering target interception
|
Xiong, Shaofeng
|
|
2015
|
|
14 |
p. 2589-2607
|
artikel
|
| 44 |
Finite-time output tracking control for air-breathing hypersonic vehicles with actuator constraints
|
An, H
|
|
2017
|
|
14 |
p. 2578-2593
|
artikel
|
| 45 |
Flow field behind a complex total pressure distortion screen
|
Sivapragasam, M
|
|
2019
|
|
14 |
p. 5075-5092
|
artikel
|
| 46 |
Flow field velocity on the flight deck of a frigate
|
Mora, Rafael Bardera
|
|
2014
|
|
14 |
p. 2674-2680
|
artikel
|
| 47 |
Flow field velocity on the flight deck of a frigate
|
Mora, Rafael Bardera
|
|
2014
|
|
14 |
p. 2674-2680
|
artikel
|
| 48 |
Fractional order fuzzy terminal sliding mode control of aerodynamics load simulator
|
Ullah, Nasim
|
|
2015
|
|
14 |
p. 2608-2619
|
artikel
|
| 49 |
Generalized optimal impact-angle-control guidance with terminal acceleration response constraint
|
Wang, Hui
|
|
2017
|
|
14 |
p. 2515-2536
|
artikel
|
| 50 |
Global performance analysis for space-based missile warning system
|
Liu, Bing
|
|
2016
|
|
14 |
p. 2569-2580
|
artikel
|
| 51 |
Guidance law with deceleration control for moving-mass reentry warhead
|
Wang, Linlin
|
|
2016
|
|
14 |
p. 2639-2653
|
artikel
|
| 52 |
Identifying pitching mode of aerial planting projectile by the use of image processing
|
Goodarzi, H
|
|
2017
|
|
14 |
p. 2616-2633
|
artikel
|
| 53 |
Improved pilot training via bifurcation analysis and robust control for aircraft loss of control problems
|
Rohith, G
|
|
2019
|
|
14 |
p. 5414-5427
|
artikel
|
| 54 |
Improving turbine endwall cooling uniformity by controlling near-wall secondary flows
|
Thomas, Mitra
|
|
2017
|
|
14 |
p. 2689-2705
|
artikel
|
| 55 |
Indirect engine sizing via distributed hybrid-electric unmanned aerial vehicle state-of-charge-based parametrisation criteria
|
Wang, S
|
|
2019
|
|
14 |
p. 5360-5368
|
artikel
|
| 56 |
Influence of struts on cavity at subsonic speeds: Flow characteristics
|
Miao, Junjie
|
|
2019
|
|
14 |
p. 5369-5379
|
artikel
|
| 57 |
Integrated guidance and control of interceptors with impact angle constraint against a high-speed maneuvering target
|
Hu, Guanjie
|
|
2019
|
|
14 |
p. 5192-5204
|
artikel
|
| 58 |
Investigations on stability and control characteristics of a CS-VLA certified aircraft using wind tunnel test data
|
Van Nguyen, Nhu
|
|
2016
|
|
14 |
p. 2728-2743
|
artikel
|
| 59 |
Lightweight and reliable metal–composite joints based on harmonization of strength properties of joined parts
|
Chernov, Andrey
|
|
2018
|
|
14 |
p. 2663-2672
|
artikel
|
| 60 |
Linearized J2 and atmospheric drag model for satellite relative motion with small eccentricity
|
Cao, Lu
|
|
2015
|
|
14 |
p. 2718-2736
|
artikel
|
| 61 |
Liquid propellant engine conceptual design by using a fuzzy-multi-objective genetic algorithm (MOGA) optimization method
|
Mirshams, M
|
|
2014
|
|
14 |
p. 2587-2603
|
artikel
|
| 62 |
Liquid propellant engine conceptual design by using a fuzzy-multi-objective genetic algorithm (MOGA) optimization method
|
Mirshams, M
|
|
2014
|
|
14 |
p. 2587-2603
|
artikel
|
| 63 |
Longitudinal coordination control of hypersonic vehicle based on dynamic equation
|
Feng, Xingkai
|
|
2019
|
|
14 |
p. 5205-5216
|
artikel
|
| 64 |
Modelling of a Scottish Aviation Bulldog using reverse engineering, wind tunnel and numerical methods
|
Lawson, NJ
|
|
2014
|
|
14 |
p. 2736-2742
|
artikel
|
| 65 |
Modelling of a Scottish Aviation Bulldog using reverse engineering, wind tunnel and numerical methods
|
Lawson, NJ
|
|
2014
|
|
14 |
p. 2736-2742
|
artikel
|
| 66 |
Motion planning of spacecraft with obstacle avoidance under low uncertainty using the improved equal-collision-probability-curve and improved linear quadratic regulator strategy
|
Yi, Wang
|
|
2019
|
|
14 |
p. 5456-5467
|
artikel
|
| 67 |
Neural-network-based real-time trajectory replanning for Mars entry guidance
|
Zheng, X
|
|
2017
|
|
14 |
p. 2634-2645
|
artikel
|
| 68 |
Numerical investigation of lateral jet interaction effects on the hypersonic quasi-waverider vehicle
|
Chai, Dong
|
|
2015
|
|
14 |
p. 2671-2680
|
artikel
|
| 69 |
Numerical investigation on staged sonic jet interaction mechanism in a supersonic cross flow
|
Huang, Wei
|
|
2014
|
|
14 |
p. 2641-2651
|
artikel
|
| 70 |
Numerical investigation on staged sonic jet interaction mechanism in a supersonic cross flow
|
Huang, Wei
|
|
2014
|
|
14 |
p. 2641-2651
|
artikel
|
| 71 |
Numerical investigation on thermo-acoustic effects and flow characteristics in semi-conical Hartmann–Sprenger resonance tube
|
Afzali, Babak
|
|
2017
|
|
14 |
p. 2706-2722
|
artikel
|
| 72 |
Numerical study of hot launch of missile inside a tube
|
Sinha, PK
|
|
2014
|
|
14 |
p. 2604-2611
|
artikel
|
| 73 |
Numerical study of hot launch of missile inside a tube
|
Sinha, PK
|
|
2014
|
|
14 |
p. 2604-2611
|
artikel
|
| 74 |
Numerical study of the unsteady behaviors and rotating stall inception process in a counter-rotating axial compressor
|
Mao, Xiaochen
|
|
2016
|
|
14 |
p. 2716-2727
|
artikel
|
| 75 |
Optimal control for far-distance rapid cooperative rendezvous
|
Feng, Wei-ming
|
|
2014
|
|
14 |
p. 2662-2673
|
artikel
|
| 76 |
Optimal control for far-distance rapid cooperative rendezvous
|
Feng, Wei-ming
|
|
2014
|
|
14 |
p. 2662-2673
|
artikel
|
| 77 |
Optimal scheduling for aerial recovery of multiple unmanned aerial vehicles using genetic algorithm
|
Liu, Yongbei
|
|
2019
|
|
14 |
p. 5347-5359
|
artikel
|
| 78 |
Optimum area of solar array for stratospheric solar-powered airship
|
Li, Jun
|
|
2017
|
|
14 |
p. 2654-2665
|
artikel
|
| 79 |
Output feedback observer-based dynamic surface controller for quadrotor UAV using quaternion representation
|
Dou, Jingxin
|
|
2017
|
|
14 |
p. 2537-2548
|
artikel
|
| 80 |
Performance analysis of aircraft fuel tank inerting system with turbocharger
|
Li, Chaoyue
|
|
2019
|
|
14 |
p. 5217-5226
|
artikel
|
| 81 |
Performance improvement of transonic centrifugal compressors by optimization of complex three-dimensional features
|
He, Xiao
|
|
2017
|
|
14 |
p. 2723-2738
|
artikel
|
| 82 |
Positioning control for an unmanned airship using sliding mode control based on fuzzy approximation
|
Yang, Yueneng
|
|
2014
|
|
14 |
p. 2627-2640
|
artikel
|
| 83 |
Positioning control for an unmanned airship using sliding mode control based on fuzzy approximation
|
Yang, Yueneng
|
|
2014
|
|
14 |
p. 2627-2640
|
artikel
|
| 84 |
Prediction of transient vibration response of dual-rotor-blade-casing system with blade off
|
Wang, Nanfei
|
|
2019
|
|
14 |
p. 5164-5176
|
artikel
|
| 85 |
Preliminary design and optimization for fleet to be used in the Small Air Transport system
|
Iwaniuk, Andrzej
|
|
2018
|
|
14 |
p. 2615-2626
|
artikel
|
| 86 |
Rapid trajectory optimization for hypersonic entry using a pseudospectral-convex algorithm
|
Wang, Jinbo
|
|
2019
|
|
14 |
p. 5227-5238
|
artikel
|
| 87 |
Real-time relative orbit estimation of noncooperative space target based on nonlinear filtering
|
Zhu, Zhenglong
|
|
2016
|
|
14 |
p. 2700-2715
|
artikel
|
| 88 |
Research on the effect of cowl lip angle on the accelerating start process of a two-dimensional hypersonic inlet
|
Xiong, Liu
|
|
2016
|
|
14 |
p. 2615-2627
|
artikel
|
| 89 |
Retuning the actuator proportional–integral–derivative controller of spinning missiles
|
Zhou, Wei
|
|
2017
|
|
14 |
p. 2594-2602
|
artikel
|
| 90 |
Review of cavity-stabilized combustion for scramjet applications
|
Wang, Zhenguo
|
|
2014
|
|
14 |
p. 2718-2735
|
artikel
|
| 91 |
Review of cavity-stabilized combustion for scramjet applications
|
Wang, Zhenguo
|
|
2014
|
|
14 |
p. 2718-2735
|
artikel
|
| 92 |
Roles of vanes in diffuser on stability of centrifugal compressor
|
Zou, Wangzhi
|
|
2019
|
|
14 |
p. 5380-5392
|
artikel
|
| 93 |
Self-adaptive phase compensation characteristics and safeguard-phase-margin design of an unsymmetrical current-sensing resistor for magnetically suspended flywheels
|
Ren, Yuan
|
|
2017
|
|
14 |
p. 2549-2559
|
artikel
|
| 94 |
Semi-analytical range and endurance computation of battery-powered multi-copter unmanned aerial systems under steady wind conditions
|
Godbole, Ameya
|
|
2019
|
|
14 |
p. 5282-5294
|
artikel
|
| 95 |
Simple frigate shape plasma flow control
|
Bardera-Mora, R
|
|
2016
|
|
14 |
p. 2693-2699
|
artikel
|
| 96 |
Structural sizing for the weight estimation of a very light aircraft wing
|
Benaouali, Abdelkader
|
|
2018
|
|
14 |
p. 2681-2687
|
artikel
|
| 97 |
Surface roughness of real operationally used compressor blade and blisk
|
Gilge, Philipp
|
|
2019
|
|
14 |
p. 5321-5330
|
artikel
|
| 98 |
Switched H2-state-feedback control with application to a fighter aircraft
|
Kemer, Emre
|
|
2019
|
|
14 |
p. 5428-5437
|
artikel
|
| 99 |
The aeroelastic characteristics of high aspect ratio wing
|
Yang, Fan
|
|
2016
|
|
14 |
p. 2543-2556
|
artikel
|
| 100 |
The composite hierarchical control of multi-link multi-DOF space manipulator based on UDE and improved sliding mode control
|
Chu, ZhongYi
|
|
2015
|
|
14 |
p. 2646-2658
|
artikel
|
| 101 |
The effect of representative bird model and its impact direction on crashworthiness of aircraft windshield and canopy structure
|
Dar, Uzair A
|
|
2019
|
|
14 |
p. 5150-5163
|
artikel
|
| 102 |
Theoretical and experimental studies on the motion and thermal states of oil droplet in a bearing chamber
|
Sun, Hengchao
|
|
2016
|
|
14 |
p. 2596-2614
|
artikel
|
| 103 |
Three-dimensional modeling and time-delay stability analysis for robotics docking simulation
|
Sazawal, Prateek
|
|
2019
|
|
14 |
p. 5438-5455
|
artikel
|
| 104 |
Three-dimensional suboptimal guidance law based on θ – D technique and nonlinear disturbance observer
|
Man, Chaoyuan
|
|
2019
|
|
14 |
p. 5122-5133
|
artikel
|
| 105 |
Thrust control of tethered satellite with a short constant tether in orbital maneuvering
|
Zhao, Guowei
|
|
2014
|
|
14 |
p. 2569-2586
|
artikel
|
| 106 |
Thrust control of tethered satellite with a short constant tether in orbital maneuvering
|
Zhao, Guowei
|
|
2014
|
|
14 |
p. 2569-2586
|
artikel
|
| 107 |
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model
|
Yang, Chen
|
|
2019
|
|
14 |
p. 5239-5252
|
artikel
|
| 108 |
Unified low-pressure compressor concept for engines of future high-speed micro-unmanned aerial vehicles
|
İlhan, Menal
|
|
2019
|
|
14 |
p. 5264-5281
|
artikel
|
| 109 |
Unsteady aerodynamic modeling based on fuzzy scalar radial basis function neural networks
|
Wang, Xu
|
|
2019
|
|
14 |
p. 5107-5121
|
artikel
|
| 110 |
Using aircraft as wind sensors for estimating accurate wind fields for air traffic management applications
|
Guadaño, Laura Hernando
|
|
2014
|
|
14 |
p. 2681-2694
|
artikel
|
| 111 |
Using aircraft as wind sensors for estimating accurate wind fields for air traffic management applications
|
Guadaño, Laura Hernando
|
|
2014
|
|
14 |
p. 2681-2694
|
artikel
|
| 112 |
Utilization of modal stress approach in random-vibration fatigue evaluation
|
Zhou, Yadong
|
|
2017
|
|
14 |
p. 2603-2615
|
artikel
|
| 113 |
Vibration analysis of a rotating variable thickness bladed disk for aircraft gas turbine engine using generalized differential quadrature method
|
Shahriari, B
|
|
2017
|
|
14 |
p. 2739-2749
|
artikel
|
| 114 |
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