| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A cognitive agent aboard remotely piloted aircraft systems: Development, evaluation, and certification issues
|
Wohler, Marcus
|
|
2016
|
|
9 |
p. 1694-1704
|
artikel
|
| 2 |
Adaptive multivariable generalized super-twisting algorithm based robust coordinated control for a space robot subjected to coupled uncertainties
|
Wei, Jinyuan
|
|
2019
|
|
9 |
p. 3244-3259
|
artikel
|
| 3 |
Advanced controller support tools for sequencing and merging operations
|
Frontera, Guillermo
|
|
2016
|
|
9 |
p. 1733-1746
|
artikel
|
| 4 |
A dynamic pressure-sink method for improving large eddy simulation and hybrid Reynolds-averaged Navier–Stokes/large eddy simulation of wall-bounded flows
|
Wang, H
|
|
2012
|
|
9 |
p. 1107-1120
|
artikel
|
| 5 |
Aerodynamic optimization design of aspirated highly loaded fan stage
|
Zhang, Jinhuan
|
|
2019
|
|
9 |
p. 3426-3444
|
artikel
|
| 6 |
Aerodynamic pitch control design for reversal of missile’s flight direction
|
Kim, Yoonsoo
|
|
2014
|
|
9 |
p. 1519-1527
|
artikel
|
| 7 |
A fast multiobjective optimization approach to S-duct scoop inlets design with both inflow and outflow
|
Zeng, Lifang
|
|
2019
|
|
9 |
p. 3381-3394
|
artikel
|
| 8 |
A finite-time-convergent composite guidance law with strong fault-tolerant performance
|
Chen, Feng
|
|
2019
|
|
9 |
p. 3120-3130
|
artikel
|
| 9 |
Air traffic generation for new terminal area air traffic management concepts design and evaluation
|
Besada, Juan
|
|
2016
|
|
9 |
p. 1721-1732
|
artikel
|
| 10 |
Algorithms for control of arrival and departure traffic in terminal airspace
|
Erzberger, Heinz
|
|
2016
|
|
9 |
p. 1762-1779
|
artikel
|
| 11 |
Altitude and attitude active disturbance rejection controller design of a quadrotor unmanned aerial vehicle
|
Dou, Jingxin
|
|
2017
|
|
9 |
p. 1732-1745
|
artikel
|
| 12 |
An adaptive wavelet collocation method for solving optimal control problem
|
Zhang, Qingbin
|
|
2015
|
|
9 |
p. 1640-1649
|
artikel
|
| 13 |
A new analytical model for reliability analysis of a launch vehicle system with limited test data
|
Murugesan, V
|
|
2019
|
|
9 |
p. 3482-3495
|
artikel
|
| 14 |
A new homing guidance law to reduce sensitivity on initial heading errors
|
Shin, Hyo-Sang
|
|
2015
|
|
9 |
p. 1740-1753
|
artikel
|
| 15 |
A new star pattern identification technique using an improved triangle algorithm
|
Li, Xin-lu
|
|
2015
|
|
9 |
p. 1730-1739
|
artikel
|
| 16 |
An experimental study of binary lateral jets on a standard model in subsonic, transonic, and supersonic cross-flows
|
Doolabi, Mostafa Hadi
|
|
2019
|
|
9 |
p. 3141-3152
|
artikel
|
| 17 |
Application of an automated aircraft architecture generation and analysis tool to unmanned aerial vehicle subsystem design
|
Judt, David M
|
|
2015
|
|
9 |
p. 1690-1708
|
artikel
|
| 18 |
Approximate analytical solutions of an axially moving spacecraft appendage subjected to tip mass
|
Ghaleh, P Bagheri
|
|
2014
|
|
9 |
p. 1487-1497
|
artikel
|
| 19 |
A preliminary method to estimate impacts of inlet flow distortion on boundary layer ingesting propulsion system design point performance
|
Liu, Chengyuan
|
|
2014
|
|
9 |
p. 1528-1539
|
artikel
|
| 20 |
A preliminary multidisciplinary design procedure for tactical missiles
|
Khalil, Mostafa
|
|
2019
|
|
9 |
p. 3445-3458
|
artikel
|
| 21 |
A self-separation algorithm for width-limited high density air corridor*
|
Nakamura, Yoichi
|
|
2016
|
|
9 |
p. 1632-1640
|
artikel
|
| 22 |
A solution to detect and avoid conflicts for civil remotely piloted aircraft systems into non-segregated airspaces
|
Migliaccio, Giovanni
|
|
2016
|
|
9 |
p. 1655-1667
|
artikel
|
| 23 |
A study on the thrust vector control using a bypass flow passage
|
Deng, R
|
|
2015
|
|
9 |
p. 1722-1729
|
artikel
|
| 24 |
Ballistic error propagation algorithm for glide trajectory based on perturbation theory
|
Zhou, Huan
|
|
2017
|
|
9 |
p. 1574-1592
|
artikel
|
| 25 |
Benefit optimization and operational requirement of Flow Corridor in Japanese airspace
|
Takeichi, Noboru
|
|
2016
|
|
9 |
p. 1780-1787
|
artikel
|
| 26 |
Bond graph modeling of a jet engine with electric starter
|
Montazeri-Gh, Morteza
|
|
2019
|
|
9 |
p. 3193-3210
|
artikel
|
| 27 |
Boundary layer suction for high-speed air intakes: A review
|
Sepahi-Younsi, Javad
|
|
2019
|
|
9 |
p. 3459-3481
|
artikel
|
| 28 |
Buffeting mitigation using carbon nanotube composites: a feasibility study
|
Yuan, Jie
|
|
2013
|
|
9 |
p. 1425-1440
|
artikel
|
| 29 |
Command filtered back-stepping control of a flexible air-breathing hypersonic flight vehicle
|
Ji, Yuehui
|
|
2014
|
|
9 |
p. 1617-1626
|
artikel
|
| 30 |
Concept description and assessment of the main features of a geared intercooled reversed flow core engine
|
Camilleri, William
|
|
2015
|
|
9 |
p. 1631-1639
|
artikel
|
| 31 |
Conceptual design of a habitation module for a deep space exploration mission
|
Viscio, Maria Antonietta
|
|
2013
|
|
9 |
p. 1389-1411
|
artikel
|
| 32 |
Conceptual development of an advanced air traffic controller workstation based on objective workload monitoring and augmented reality
|
Rohacs, Jozsef
|
|
2016
|
|
9 |
p. 1747-1761
|
artikel
|
| 33 |
Control system design for hypersonic reentry vehicle driven by aerosurfaces and reaction control system
|
Cai, Gaohua
|
|
2015
|
|
9 |
p. 1575-1587
|
artikel
|
| 34 |
Conventional helicopters: an adaptiveness study for more electric and alternative propulsion technologies
|
Buysschaert, F
|
|
2012
|
|
9 |
p. 1078-1094
|
artikel
|
| 35 |
Cooperative guidance law considering the randomness of the unreliable communication network
|
Zhang, Chunyan
|
|
2019
|
|
9 |
p. 3313-3322
|
artikel
|
| 36 |
Coupled orbital and attitude control in spacecraft rendezvous and soft docking
|
Yang, Yaguang
|
|
2019
|
|
9 |
p. 3109-3119
|
artikel
|
| 37 |
Cross-entropy-based cost-efficient 4D trajectory generation for airborne conflict resolution
|
Koyuncu, Emre
|
|
2016
|
|
9 |
p. 1605-1631
|
artikel
|
| 38 |
Defining dynamic route structure for airspace configuration
|
Zelinski, S
|
|
2012
|
|
9 |
p. 1161-1170
|
artikel
|
| 39 |
Designing freedom into trajectory-based operations
|
Kuenz, Alexander
|
|
2016
|
|
9 |
p. 1558-1568
|
artikel
|
| 40 |
Design of hypersonic forebody with submerged bump
|
Saheby, Eiman B
|
|
2019
|
|
9 |
p. 3153-3169
|
artikel
|
| 41 |
Design of UAV for photogrammetric mission in Antarctic area
|
Goetzendorf-Grabowski, Tomasz
|
|
2017
|
|
9 |
p. 1660-1675
|
artikel
|
| 42 |
Design optimization of aerodynamic shapes of a wing and its winglet using modified quantum-behaved particle swarm optimization algorithm
|
Wei, Zhang
|
|
2014
|
|
9 |
p. 1638-1647
|
artikel
|
| 43 |
Development of an off-design deviation angle prediction model for full blade span in axial flow compressors
|
Wu, Dongrun
|
|
2019
|
|
9 |
p. 3170-3183
|
artikel
|
| 44 |
Development of body force model for steady inlet distortions in high-speed multistage compressor
|
Guo, Jin
|
|
2017
|
|
9 |
p. 1650-1659
|
artikel
|
| 45 |
Distributed efficiency-based circular formation for the unmanned air vehicles detection system
|
Zilun, Hu
|
|
2019
|
|
9 |
p. 3223-3234
|
artikel
|
| 46 |
Distributed finite-time configuration containment control for satellite formation
|
Sun, Yanchao
|
|
2017
|
|
9 |
p. 1609-1620
|
artikel
|
| 47 |
Dynamic modeling and fuzzy control for a small tiltrotor unmanned aerial vehicle
|
Chang, Sungho
|
|
2013
|
|
9 |
p. 1468-1487
|
artikel
|
| 48 |
Dynamic optimal UAV trajectory planning in the National Airspace System via mixed integer linear programming
|
Radmanesh, Mohammadreza
|
|
2016
|
|
9 |
p. 1668-1682
|
artikel
|
| 49 |
Dynamic pressure based mid-course guidance scheme for hypersonic boost-glide vehicle
|
Kumar, G Naresh
|
|
2019
|
|
9 |
p. 3211-3222
|
artikel
|
| 50 |
Effect of jet noise reduction on gas turbine engine efficiency
|
Doulgeris, Georgios
|
|
2013
|
|
9 |
p. 1441-1455
|
artikel
|
| 51 |
Effect of titanium nitride coating for improvement of fire resistivity of polymer composites for aerospace application
|
Venkatesan, Ganesh
|
|
2018
|
|
9 |
p. 1692-1703
|
artikel
|
| 52 |
Effects of blade rotation on axial turbine tip leakage vortex breakdown and loss
|
Gao, Jie
|
|
2017
|
|
9 |
p. 1634-1649
|
artikel
|
| 53 |
Efficient global optimization for S-duct diffuser shape design
|
Bae, HyoGil
|
|
2013
|
|
9 |
p. 1516-1532
|
artikel
|
| 54 |
Empirical analysis of aircraft clusters in air traffic situation networks
|
Wang, Hongyong
|
|
2017
|
|
9 |
p. 1718-1731
|
artikel
|
| 55 |
Enhanced situation awareness for unmanned aerial vehicle operating in terminal areas with circuit flight rules
|
Liu, Cunjia
|
|
2016
|
|
9 |
p. 1683-1693
|
artikel
|
| 56 |
Evaluating the local environmental impact of air traffic with air transport systems evaluation infrastructure: outputs and validation walkthrough
|
Aubry, S
|
|
2012
|
|
9 |
p. 1192-1200
|
artikel
|
| 57 |
Experimental investigation of the dynamic stall phenomenon on a NACA 23012 oscillating airfoil
|
Zanotti, Alex
|
|
2013
|
|
9 |
p. 1375-1388
|
artikel
|
| 58 |
Experimental investigation of the icing scaling test method for a rotating cone
|
Zhang, Fei
|
|
2019
|
|
9 |
p. 3368-3380
|
artikel
|
| 59 |
Experimental investigation on ignition limits of plasma-assisted ignition in the propane–air mixture
|
Yu, Jinlu
|
|
2018
|
|
9 |
p. 1685-1691
|
artikel
|
| 60 |
Experimental investigation on separation control by slot jet in highly loaded compressor cascade
|
Jiaguo, Hu
|
|
2018
|
|
9 |
p. 1704-1714
|
artikel
|
| 61 |
Experimental study of flow field on stepped airfoil at very low Reynolds number
|
Kamyab Matin, Reza
|
|
2017
|
|
9 |
p. 1706-1717
|
artikel
|
| 62 |
Explicit non-linear model predictive control for autonomous helicopters
|
Liu, C
|
|
2012
|
|
9 |
p. 1171-1182
|
artikel
|
| 63 |
Extension local representation of gravity anomaly along glide trajectory
|
Zhou, Huan
|
|
2018
|
|
9 |
p. 1764-1786
|
artikel
|
| 64 |
Fault tree analysis for composite structural damages
|
Chen, Xi
|
|
2014
|
|
9 |
p. 1466-1474
|
artikel
|
| 65 |
Feasibility study on a neutron diffraction method for non-destructive evaluation of residual strain distribution of a combustion chamber
|
Moriya, S
|
|
2012
|
|
9 |
p. 1139-1146
|
artikel
|
| 66 |
Flight controller learning based on real-time model estimation of a quadrotor aircraft
|
Alabsi, Mohammed
|
|
2019
|
|
9 |
p. 3298-3312
|
artikel
|
| 67 |
Flight testing of noise abating required navigation performance procedures and steep approaches
|
Toebben, Helmut H
|
|
2014
|
|
9 |
p. 1586-1597
|
artikel
|
| 68 |
Flow control via instabilities, vortices and steady structures under the action of external microwave energy release
|
Azarova, Olga
|
|
2013
|
|
9 |
p. 1498-1515
|
artikel
|
| 69 |
Formal verification of lateral and temporal safety buffers for state-based conflict detection
|
Narkawicz, Anthony
|
|
2013
|
|
9 |
p. 1412-1424
|
artikel
|
| 70 |
Geomagnetic gradient bionic navigation based on the parallel approaching method
|
Jun, Zhou
|
|
2019
|
|
9 |
p. 3131-3140
|
artikel
|
| 71 |
Huber-based divided difference filter with application to relative navigation
|
Li, Wei
|
|
2014
|
|
9 |
p. 1475-1486
|
artikel
|
| 72 |
Hybrid systems modeling and automated air traffic control for three-dimensional separation assurance
|
Pasaoglu, Cengiz
|
|
2016
|
|
9 |
p. 1788-1809
|
artikel
|
| 73 |
Improved criteria for stall-free preliminary design of axial compressor of aero gas turbine engines
|
Aligoodarz, MR
|
|
2019
|
|
9 |
p. 3286-3297
|
artikel
|
| 74 |
Improved disturbance rejection control based on H∞ synthesis and equivalent-input-disturbance for aircraft longitudinal autopilot design
|
Li, Tong
|
|
2019
|
|
9 |
p. 3323-3335
|
artikel
|
| 75 |
In-flight performance analysis of a non-cooperative radar-based sense and avoid system
|
Fasano, Giancarmine
|
|
2016
|
|
9 |
p. 1592-1604
|
artikel
|
| 76 |
Influence of multi-wall separation control on normal-shock-induced separation in supersonic duct flows
|
Vaisakh, S
|
|
2019
|
|
9 |
p. 3184-3192
|
artikel
|
| 77 |
Influence of nozzle configuration on the flow field of multiple jets
|
Kannan, BT
|
|
2018
|
|
9 |
p. 1639-1654
|
artikel
|
| 78 |
Influence of open trailing edge on laminar aerofoils at low Reynolds number
|
Sant, Rodolfo
|
|
2013
|
|
9 |
p. 1456-1467
|
artikel
|
| 79 |
Integrated guidance and control based on block backstepping sliding mode and dynamic control allocation
|
Guo, Chao
|
|
2015
|
|
9 |
p. 1559-1574
|
artikel
|
| 80 |
Investigation on the anti-regulation characteristic of variable flow ducted rocket
|
Ma, Li-Kun
|
|
2013
|
|
9 |
p. 1488-1497
|
artikel
|
| 81 |
Investigations on supersonic combustion in a combustion-driven shock tunnel
|
Ratan, J
|
|
2012
|
|
9 |
p. 1183-1191
|
artikel
|
| 82 |
Liquid-propellant rocket engine online health condition monitoring base on multi-algorithm parallel integrated decision-making
|
Nie, Yao
|
|
2017
|
|
9 |
p. 1621-1633
|
artikel
|
| 83 |
Longitudinal nonlinear adaptive autopilot design for missiles with control constraint
|
Lee, Keum W
|
|
2018
|
|
9 |
p. 1655-1670
|
artikel
|
| 84 |
Micro-electromechanical systems gyro performance improvement through bias correction over temperature using an adaptive neural network-trained fuzzy inference system
|
Grigorie, T L
|
|
2012
|
|
9 |
p. 1121-1138
|
artikel
|
| 85 |
Minimal modelling approach to describe turbulent rocket roll dynamics in a vertical wind tunnel
|
Hann, C E
|
|
2012
|
|
9 |
p. 1042-1060
|
artikel
|
| 86 |
Modal characteristics and unbalance responses of fan rotor system with flexible support structures in aero-engine
|
Wang, Meiling
|
|
2017
|
|
9 |
p. 1686-1705
|
artikel
|
| 87 |
Modeling and control of a torque load system with servo actuator's dynamics
|
Wang, Xin
|
|
2017
|
|
9 |
p. 1676-1685
|
artikel
|
| 88 |
Modification of Leishman–Beddoes model incorporating with a new trailing-edge vortex model
|
Wang, Qing
|
|
2015
|
|
9 |
p. 1606-1615
|
artikel
|
| 89 |
Multi-model approaches to three-axis missile autopilot design under aerodynamic roll angle uncertainty
|
Won, D-Y
|
|
2012
|
|
9 |
p. 1061-1077
|
artikel
|
| 90 |
Multi-objective optimization of a composite wing subject to strength and aeroelastic constraints
|
Guo, S
|
|
2012
|
|
9 |
p. 1095-1106
|
artikel
|
| 91 |
Multiobjective optimization of hard coating parameters designing for damping of the bladed disk
|
Chen, Yugang
|
|
2018
|
|
9 |
p. 1609-1619
|
artikel
|
| 92 |
Non-equatorial space elevator design approach
|
Wang, Z-K
|
|
2019
|
|
9 |
p. 3235-3243
|
artikel
|
| 93 |
Nonlinear adaptive trajectory tracking control for a quad-rotor with parametric uncertainty
|
Sun, Liang
|
|
2015
|
|
9 |
p. 1709-1721
|
artikel
|
| 94 |
Nonlinear aerodynamic model identification using empirical mode decomposition
|
Bagherzadeh, SA
|
|
2015
|
|
9 |
p. 1588-1605
|
artikel
|
| 95 |
Nonlinear cooperative UAV maneuvers in pitch plane
|
Ashokkumar, Chimpalthradi R
|
|
2017
|
|
9 |
p. 1746-1755
|
artikel
|
| 96 |
Non-linear idealisation error analysis of an aerospace stiffened panel loaded in compression
|
Hetey, Laszlo
|
|
2014
|
|
9 |
p. 1574-1585
|
artikel
|
| 97 |
Nonlinear vibration control of a membrane antenna structure
|
Liu, Xiang
|
|
2019
|
|
9 |
p. 3273-3285
|
artikel
|
| 98 |
Numerical analysis of a swept wing hot air ice protection system
|
Bu, Xueqin
|
|
2014
|
|
9 |
p. 1507-1518
|
artikel
|
| 99 |
Numerical investigation of hypersonic flow with repetitive-pulsed plasma actuators
|
Wang, Chin-Cheng
|
|
2018
|
|
9 |
p. 1715-1724
|
artikel
|
| 100 |
On a dimensionless alternative to the ICAO target level of safety
|
Campos, LMBC
|
|
2016
|
|
9 |
p. 1548-1557
|
artikel
|
| 101 |
Optimal patterns of dynamic soaring with a small unmanned aerial vehicle
|
Liu, Duo-Neng
|
|
2017
|
|
9 |
p. 1593-1608
|
artikel
|
| 102 |
Optimal preliminary design of electromechanical actuators
|
Budinger, Marc
|
|
2014
|
|
9 |
p. 1598-1616
|
artikel
|
| 103 |
Optimization design of unitized panels with stiffeners in different formats using the evolutionary strategy with covariance matrix adaptation
|
Yang, Weizhu
|
|
2017
|
|
9 |
p. 1563-1573
|
artikel
|
| 104 |
Optimization of flapping wing mechanism of bionic eagle
|
Huang, Mingyang
|
|
2019
|
|
9 |
p. 3260-3272
|
artikel
|
| 105 |
Parametric study of the effect of exothermic coating properties on blunt nose drag reduction in hypersonic flights
|
Tahsini, AmirMahdi
|
|
2014
|
|
9 |
p. 1461-1465
|
artikel
|
| 106 |
Preliminary design and comparative study of thermal control in a nanosatellite through smart variable emissivity surfaces
|
Athanasopoulos, N
|
|
2019
|
|
9 |
p. 3336-3350
|
artikel
|
| 107 |
Preliminary reliability analysis of a high-altitude airship’s envelope
|
Liu, Jian
|
|
2014
|
|
9 |
p. 1648-1653
|
artikel
|
| 108 |
Researches on inverse simulation’s applications in teleoperation rendezvous and docking based on hyper-ellipsoidal restricted model predictive control for inverse simulation structure
|
Zhou, Wanmeng
|
|
2015
|
|
9 |
p. 1675-1689
|
artikel
|
| 109 |
Research on advanced flight control methods based on actuator constraints for elastic model of hypersonic vehicle
|
Liu, Yan-bin
|
|
2014
|
|
9 |
p. 1627-1637
|
artikel
|
| 110 |
Reynolds averaged Navier-Stokes simulations of compressible mixing layers of similar and dissimilar gases: Performance of k–ɛ turbulence model
|
Javed, Afroz
|
|
2015
|
|
9 |
p. 1650-1660
|
artikel
|
| 111 |
Robust finite time second-order sliding mode stabilization control for floated inertial platform
|
Yu, Chunmei
|
|
2018
|
|
9 |
p. 1620-1627
|
artikel
|
| 112 |
Shape optimization of airfoils in transonic flow using a multi-objective genetic algorithm
|
Chen, Xiaomin
|
|
2014
|
|
9 |
p. 1654-1667
|
artikel
|
| 113 |
Single sensor-based 3D feature point location for a small flying robot application using one camera
|
Shah, Syed Irtiza Ali
|
|
2014
|
|
9 |
p. 1668-1689
|
artikel
|
| 114 |
Special Issue on Air Traffic Management
|
Di Vito, Vittorio
|
|
2016
|
|
9 |
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