| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A conceptual method to assess ship-helicopter dynamic interface
|
Shukla, Shrish
|
|
|
|
5 |
p. 1092-1116
|
artikel
|
| 2 |
A coordinated turn controller for a fixed-wing aircraft
|
Corona-Sánchez, José J
|
|
2019
|
|
5 |
p. 1728-1740
|
artikel
|
| 3 |
Adaptive command filtered backstepping tracking controller design for quadrotor unmanned aerial vehicle
|
Choi, In-Ho
|
|
2012
|
|
5 |
p. 483-497
|
artikel
|
| 4 |
Adaptive fuzzy fault-tolerant control for rigid spacecraft attitude maneuver with finite-time convergence
|
Ran, Dechao
|
|
2016
|
|
5 |
p. 779-792
|
artikel
|
| 5 |
Adaptive nonsingular terminal sliding mode guidance law against maneuvering targets with impact angle constraint
|
Wang, Weihong
|
|
2015
|
|
5 |
p. 867-890
|
artikel
|
| 6 |
A distribution model of the GNSS code noise and multipath error considering both elevation angle and orbit type
|
Fan, Guochao
|
|
2019
|
|
5 |
p. 1900-1915
|
artikel
|
| 7 |
A 3D pitch and impact-angle constrained guidance scheme
|
Varma, S Aditya
|
|
2019
|
|
5 |
p. 1571-1584
|
artikel
|
| 8 |
Aerodynamic characteristics of breathing blunt nose configuration at hypersonic speeds
|
Watanabe, Yasumasa
|
|
2017
|
|
5 |
p. 840-858
|
artikel
|
| 9 |
Aerodynamic coupling model development and autopilot design for highly manoeuvring skid-to-turn missiles
|
Kim, S-H
|
|
2012
|
|
5 |
p. 498-509
|
artikel
|
| 10 |
Aerodynamic performance analysis and optimization of a turbine duct with low degree of partial admission
|
Sui, Xiuming
|
|
2018
|
|
5 |
p. 988-1001
|
artikel
|
| 11 |
Aerodynamic performance of a two-dimensional flapping wing in asymmetric stroke
|
Zhu, JY
|
|
2014
|
|
5 |
p. 641-651
|
artikel
|
| 12 |
Aeroelastic analysis of twin turboprop utility aircraft
|
Cecrdle, J.
|
|
2011
|
|
5 |
p. 585-594
|
artikel
|
| 13 |
Aeroelastic numerical approach of a wing based on the finite element and boundary element methods
|
Dehkordi, Iman Roohi
|
|
2013
|
|
5 |
p. 882-894
|
artikel
|
| 14 |
A fast mutant fault detection method of underwater integrated navigation
|
Liu, Yi-ting
|
|
2016
|
|
5 |
p. 815-831
|
artikel
|
| 15 |
Aircraft used as a sensor for atmospheric behaviour determination. Practical case: pressure estimation using automatic dependent surveillance-broadcast
|
Alarcón, José F Alonso
|
|
2013
|
|
5 |
p. 778-797
|
artikel
|
| 16 |
Almost global trajectory tracking control of quadrotors with constrained control inputs
|
Zuo, Zongyu
|
|
2016
|
|
5 |
p. 856-869
|
artikel
|
| 17 |
Analysis of uncertainties in measurement of rotor blade tip clearance in gas turbine engine under dynamic condition
|
Satish, TN
|
|
2014
|
|
5 |
p. 652-670
|
artikel
|
| 18 |
Analytical analysis of vibration characteristics for the hard-coating cantilever laminated plate
|
Sun, Wei
|
|
2018
|
|
5 |
p. 813-824
|
artikel
|
| 19 |
Analytical study of stationary temperature field in transpiration cooled porous wall
|
Zhukov, Victor P
|
|
2013
|
|
5 |
p. 873-881
|
artikel
|
| 20 |
Analytic solutions of optimal angularly constrained guidance for first-order lag system
|
Lee, Yong-In
|
|
2013
|
|
5 |
p. 827-837
|
artikel
|
| 21 |
Analytic study of the conditions required for longitudinal stability of dual-wing aircraft
|
Andrews, SA
|
|
2018
|
|
5 |
p. 958-972
|
artikel
|
| 22 |
An efficient extended target detection method based on region growing and contour tracking algorithm
|
Yan, Bo
|
|
2018
|
|
5 |
p. 825-836
|
artikel
|
| 23 |
A new curvature-controlled stacking-line method for optimization design of compressor cascade considering surface smoothness
|
Zhang, Xinyi
|
|
|
|
5 |
p. 1061-1074
|
artikel
|
| 24 |
A new method for design of fixed wing micro air vehicle
|
Hassanalian, Mostafa
|
|
2015
|
|
5 |
p. 837-850
|
artikel
|
| 25 |
An experimental and numerical study of piezoceramic actuator hysteresis in helicopter active vibration control
|
Mallick, Rajnish
|
|
2014
|
|
5 |
p. 690-705
|
artikel
|
| 26 |
An improved streamline curvature approach for transonic axial compressor performance prediction
|
Hu, J.F.
|
|
2011
|
|
5 |
p. 575-584
|
artikel
|
| 27 |
An integral sliding mode controller based disturbances rejection compound scheme for inertially stabilized platform in aerial remote sensing
|
Zhou, Xiangyang
|
|
2018
|
|
5 |
p. 932-943
|
artikel
|
| 28 |
An integrated estimation/guidance approach for seeker-less interceptors
|
Kumar, G Saroj
|
|
2015
|
|
5 |
p. 891-905
|
artikel
|
| 29 |
A novel fault diagnosis approach based on environmental stress level evaluation
|
Deng, Guanqian
|
|
2013
|
|
5 |
p. 816-826
|
artikel
|
| 30 |
A novel guidance strategy for autonomously approaching a tumbling target
|
Ge, Juxiang
|
|
2018
|
|
5 |
p. 861-871
|
artikel
|
| 31 |
Application of Lyapunov matrix inequality based unsymmetrical saturated control to a multi-vectored propeller airship
|
Chen, Li
|
|
2018
|
|
5 |
p. 884-901
|
artikel
|
| 32 |
A practical method to account for seal friction in aircraft hydraulic actuator preliminary design
|
Agarwal, Naresh Kumar
|
|
2017
|
|
5 |
p. 941-950
|
artikel
|
| 33 |
A quadratic homotopy method for fuel-optimal low-thrust trajectory design
|
Pan, Binfeng
|
|
2019
|
|
5 |
p. 1741-1757
|
artikel
|
| 34 |
A review of numerical simulation and modeling of combustion in scramjets
|
Clark, Ryan J
|
|
2015
|
|
5 |
p. 958-980
|
artikel
|
| 35 |
A simulation environment for path and image generation in an aerial single-camera vision system
|
Amiri Atashgah, M.A.
|
|
2011
|
|
5 |
p. 541-558
|
artikel
|
| 36 |
Aspects of aero-engine nacelle drag
|
Robinson, Matthew
|
|
2019
|
|
5 |
p. 1667-1682
|
artikel
|
| 37 |
A stress analysis of a compressor blade in partially blocked inlet condition
|
Drewczynski, M
|
|
2016
|
|
5 |
p. 934-952
|
artikel
|
| 38 |
A study on the aerodynamic characteristics of a stratospheric airship in its entire flight envelope
|
Sun, Xiao-Ying
|
|
2018
|
|
5 |
p. 902-921
|
artikel
|
| 39 |
A surrogate-based integrated framework for the aerodynamic design optimization of a subsonic wing planform shape
|
Benaouali, Abdelkader
|
|
2018
|
|
5 |
p. 872-883
|
artikel
|
| 40 |
A time-space synchronized fluid-structure coupling algorithm for the prediction of wing flutter
|
Zhong, Jize
|
|
2018
|
|
5 |
p. 922-931
|
artikel
|
| 41 |
Atmospheric vehicle trajectory optimization with minimum dynamic pressure constraint
|
Kumar, G Naresh
|
|
2018
|
|
5 |
p. 837-846
|
artikel
|
| 42 |
Augmented robust control of a free-floating flexible space robot
|
Yu, Xiao-Yan
|
|
2015
|
|
5 |
p. 947-957
|
artikel
|
| 43 |
A winding machine for polarized wire grid of microwave radiometer calibration
|
Hu, Yong
|
|
2019
|
|
5 |
p. 1916-1925
|
artikel
|
| 44 |
Characteristic investigations on magnetic field and fluid field of a giant magnetostrictive material-based electro-hydrostatic actuator
|
Yang, Xulei
|
|
2018
|
|
5 |
p. 847-860
|
artikel
|
| 45 |
Comparison between bolt clamping force and composite patches for repairing aircraft structures of aluminum alloy 2024-T3
|
Maleki, HN
|
|
2019
|
|
5 |
p. 1758-1771
|
artikel
|
| 46 |
Conceptual study of a dual-rocket-based-combined-cycle powered two-stage-to-orbit launch vehicle
|
Zhang, Fan
|
|
2018
|
|
5 |
p. 944-957
|
artikel
|
| 47 |
Continuous low thrust trajectory optimization for preliminary design
|
Sun, Chong
|
|
2016
|
|
5 |
p. 921-933
|
artikel
|
| 48 |
Control-based fault detection and isolation for autonomous aircraft
|
Marzat, J
|
|
2012
|
|
5 |
p. 510-531
|
artikel
|
| 49 |
Coordinated attitude control of hypersonic flight vehicles based on the coupling analysis
|
Zhen, Wubin
|
|
2018
|
|
5 |
p. 1002-1011
|
artikel
|
| 50 |
Corrigendum
|
|
|
|
|
5 |
p. NP1
|
artikel
|
| 51 |
Corrigendum to “Numerical and experimental investigation of damage effect on a hemispherical parachute performance”
|
|
|
|
|
5 |
p. NP2
|
artikel
|
| 52 |
Decentralized robust coordinated control for formation flying spacecraft with coupled attitude and translational dynamics
|
Zhang, Bao-Qun
|
|
2013
|
|
5 |
p. 798-815
|
artikel
|
| 53 |
Design of an aerial combat guidance law using virtual pursuit point concept
|
You, Dong-Il
|
|
2015
|
|
5 |
p. 792-813
|
artikel
|
| 54 |
Design of an analytical fault tolerant attitude determination system using Euler angles and rotation matrices for a three-axis satellite
|
Bolandi, Hossein
|
|
2014
|
|
5 |
p. 706-726
|
artikel
|
| 55 |
Design optimization of a thrust chamber using a mass-based model to improve the geometrical and performance parameters of low-thrust space propulsion systems
|
Shafaee, Maziar
|
|
2019
|
|
5 |
p. 1820-1837
|
artikel
|
| 56 |
Detonation-driven–shock wave interactions with perforated plates
|
Zare-Behtash, H
|
|
2014
|
|
5 |
p. 671-678
|
artikel
|
| 57 |
Development of a new tool for constrained conflict resolution
|
Han, Yun-xiang
|
|
2019
|
|
5 |
p. 1683-1694
|
artikel
|
| 58 |
Dynamic response analysis of aero hydraulic pipeline system under pump fluid pressure fluctuation
|
Gao, Pei-xin
|
|
2019
|
|
5 |
p. 1585-1595
|
artikel
|
| 59 |
Effect of rotational direction of triple-swirler on cold flow characteristics of a model combustor
|
Zhao, Ziqiang
|
|
2017
|
|
5 |
p. 918-930
|
artikel
|
| 60 |
Effects of propeller thrust trimming on tailless unmanned aerial vehicle performance
|
Wang, Gang
|
|
2016
|
|
5 |
p. 870-885
|
artikel
|
| 61 |
Effects of revolute clearance joint on the dynamic behavior of a planar space arm system
|
Miao, Huihui
|
|
2019
|
|
5 |
p. 1629-1644
|
artikel
|
| 62 |
Effects of thermochemical modelling and surface catalyticity on an Earth re-entry vehicle
|
Viviani, A.
|
|
2011
|
|
5 |
p. 523-540
|
artikel
|
| 63 |
Energy harvesting from limit cycle oscillation of a cantilever plate in low subsonic flow by ionic polymer metal composite
|
Jamshidi, Shahab
|
|
2015
|
|
5 |
p. 814-836
|
artikel
|
| 64 |
Evaluating NOx and CO emissions of bio-SPK fuel using a simplified engine combustion model: A preliminary study towards sustainable environment
|
Mazlan, Nurul Musfirah
|
|
2017
|
|
5 |
p. 859-865
|
artikel
|
| 65 |
Experimental and numerical investigation of cavity-based supersonic flow and combustion
|
Wang, Hongbo
|
|
2014
|
|
5 |
p. 781-798
|
artikel
|
| 66 |
Experimental investigations on effects of tip clearance in mixed-flow compressor performance
|
Rajakumar, D Ramesh
|
|
2015
|
|
5 |
p. 933-946
|
artikel
|
| 67 |
Experimental study on axially non-uniform clearances in a linear turbine cascade with a cavity squealer tip
|
Chen, Shaowen
|
|
2019
|
|
5 |
p. 1645-1655
|
artikel
|
| 68 |
Fault diagnosis and robust fault-tolerant control for linear over-actuated systems
|
Zhou, Meng
|
|
2016
|
|
5 |
p. 832-844
|
artikel
|
| 69 |
Film cooling optimization on leading edge gas turbine blade using differential evolution
|
García, Juan C
|
|
2019
|
|
5 |
p. 1656-1666
|
artikel
|
| 70 |
Finite element analysis of solar sail force model with mission application
|
Boni, Luisa
|
|
2019
|
|
5 |
p. 1838-1846
|
artikel
|
| 71 |
Firing tests of hybrid engine with varying oxidiser nature and operating conditions
|
Gascoin, Nicolas
|
|
2014
|
|
5 |
p. 755-765
|
artikel
|
| 72 |
Flight operation and airframe design for tradeoff between cost and environmental impact
|
Wang, Yu
|
|
2018
|
|
5 |
p. 973-987
|
artikel
|
| 73 |
Flight test of flying-wing type unmanned aerial vehicle with partial wing-loss
|
Kim, Kijoon
|
|
2019
|
|
5 |
p. 1611-1628
|
artikel
|
| 74 |
Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
|
Correa, G
|
|
2015
|
|
5 |
p. 917-932
|
artikel
|
| 75 |
Frequency domain input identification for vibration testing of flexible structures
|
Ramkrishna, D
|
|
2013
|
|
5 |
p. 838-856
|
artikel
|
| 76 |
Fuzzy integral sliding mode based on backstepping control synthesis for an autonomous helicopter
|
Meguenni, Kadda Zemalache
|
|
2013
|
|
5 |
p. 751-765
|
artikel
|
| 77 |
Geographical area selection and construction of a corresponding routing grid used for in-flight management system flight trajectory optimization
|
Dancila, Bogdan D
|
|
2017
|
|
5 |
p. 809-822
|
artikel
|
| 78 |
Heuristics for a runway-queue management problem
|
Stiverson, P.
|
|
2011
|
|
5 |
p. 481-499
|
artikel
|
| 79 |
H∞/Predictive output control of a three-axis gyrostabilized platform
|
Darestani, Mahdy Rezaei
|
|
2014
|
|
5 |
p. 679-689
|
artikel
|
| 80 |
Identification of a non-linear F/A-18 model by the use of fuzzy logic and neural network methods
|
Boely, N.
|
|
2011
|
|
5 |
p. 559-574
|
artikel
|
| 81 |
Identification of spin maneuver aerodynamic nonlinear model by applying ensemble empirical mode decomposition and extended multipoint modeling
|
Mokhtari, MA
|
|
2019
|
|
5 |
p. 1865-1878
|
artikel
|
| 82 |
Improving in-orbit responsiveness of low earth orbit sun-synchronous satellites by selection of ground segment location
|
Navabi, M
|
|
2013
|
|
5 |
p. 766-777
|
artikel
|
| 83 |
Influence of different loads on the stresses of multistage axial compressor rotors
|
Zheng, Xinqian
|
|
2017
|
|
5 |
p. 787-798
|
artikel
|
| 84 |
Invariant set based sliding mode control for near-space vehicles with attitude constraints
|
Fu, Jian
|
|
2016
|
|
5 |
p. 793-804
|
artikel
|
| 85 |
Investigation of endwall treatment and shock control in a five-stage axial compressor
|
Yang, Heli
|
|
|
|
5 |
p. 1035-1049
|
artikel
|
| 86 |
Large deformation bending responses of nanotube-reinforced polymer composite panel structure: Numerical and experimental analyses
|
Mehar, Kulmani
|
|
2019
|
|
5 |
p. 1695-1704
|
artikel
|
| 87 |
Librational characteristics of a dumbbell modeled tethered satellite under small, continuous, constant thrust
|
Zhao, Guowei
|
|
2013
|
|
5 |
p. 857-872
|
artikel
|
| 88 |
Lift and drag on a sphere above ground by a sliding shock
|
Igra, D
|
|
2012
|
|
5 |
p. 550-560
|
artikel
|
| 89 |
Linear-parameter-varying-based adaptive sliding mode control with bounded L2 gain performance for a morphing aircraft
|
Wen, Nuan
|
|
2019
|
|
5 |
p. 1847-1864
|
artikel
|
| 90 |
Metamodel-based optimization of the bolted connection of a wing spar considering fatigue resistance
|
Xia, Tianxiang
|
|
2016
|
|
5 |
p. 805-814
|
artikel
|
| 91 |
Method for assessing combat survivability for aircraft with wing damage
|
Pei, Yang
|
|
2017
|
|
5 |
p. 877-886
|
artikel
|
| 92 |
Modelling and attitude control of a miniature ducted fan UAV
|
Zhao, Hong
|
|
2016
|
|
5 |
p. 953-964
|
artikel
|
| 93 |
Modelling electro-impulse de-icing process in leading edge structure and impact fatigue life prediction of rivet holes in critical areas
|
Zhang, Yongjie
|
|
|
|
5 |
p. 1117-1131
|
artikel
|
| 94 |
Multi-objective optimization of lean and sweep angles for stator and rotor blades of an axial turbine
|
Asgarshamsi, Abolhassan
|
|
2015
|
|
5 |
p. 906-916
|
artikel
|
| 95 |
Multiple-time scale smooth second order sliding mode controller design for flexible hypersonic vehicles
|
Tian, Bailing
|
|
2015
|
|
5 |
p. 781-791
|
artikel
|
| 96 |
Nonlinear regression Huber-based divided difference filtering
|
Li, Wei
|
|
2017
|
|
5 |
p. 799-808
|
artikel
|
| 97 |
Nonlinear system controllability analysis and autopilot design for bank-to-turn aircraft with two flaps
|
Dong, Jinlu
|
|
2019
|
|
5 |
p. 1772-1783
|
artikel
|
| 98 |
Nonsingular adaptive-gain super-twisting guidance with an impact angle constraint
|
Li, Guofei
|
|
2019
|
|
5 |
p. 1705-1714
|
artikel
|
| 99 |
NOx, fuel consumption and time effects of flight path angle during descent
|
Turgut, Enis T
|
|
2013
|
|
5 |
p. 737-750
|
artikel
|
| 100 |
Numerical analysis of flow separation and side loads of a conical nozzle during staging
|
Jia, Ruyan
|
|
2016
|
|
5 |
p. 845-855
|
artikel
|
| 101 |
Numerical and experimental investigation of damage effect on a hemispherical parachute performance
|
Etemadi, Fakhri
|
|
|
|
5 |
p. 1050-1060
|
artikel
|
| 102 |
Numerical assessment of an L-shaped Gurney flap for load control
|
Motta, Valentina
|
|
2017
|
|
5 |
p. 951-975
|
artikel
|
| 103 |
Numerical investigation on impact of blowing control in flush-mounted S-shaped inlet to rear fan-stage performance
|
Liu, Lei
|
|
2016
|
|
5 |
p. 895-905
|
artikel
|
| 104 |
Operation of a pulse detonation engine system at high frequency
|
Lu, Wei
|
|
2016
|
|
5 |
p. 886-894
|
artikel
|
| 105 |
Optimal trajectory planning for path convergence in three-dimensional space
|
Hota, Sikha
|
|
2014
|
|
5 |
p. 766-780
|
artikel
|
| 106 |
Optimization of area navigation noise abatement approach trajectories
|
Hogenhuis, R.H.
|
|
2011
|
|
5 |
p. 513-521
|
artikel
|
| 107 |
Parametric study of sensitivity of deployed frequency for large cable net antenna
|
Balaji, K
|
|
2014
|
|
5 |
p. 727-739
|
artikel
|
| 108 |
Pilot modeling based on time-delay synthesis
|
Toader, Adrian
|
|
2014
|
|
5 |
p. 740-754
|
artikel
|
| 109 |
Planar path following nonlinear controller design for an autonomous airship
|
Zhou, Wei-xiang
|
|
2019
|
|
5 |
p. 1879-1899
|
artikel
|
| 110 |
Prediction of airfoil noise induced by low-Mach-number flow
|
Mao, Y
|
|
2012
|
|
5 |
p. 561-573
|
artikel
|
| 111 |
Predictions of NOx and CO emissions from a low-emission concentric staged combustor for civil aeroengines
|
Zhang, Qun
|
|
|
|
5 |
p. 1075-1091
|
artikel
|
| 112 |
Preliminary suitability analysis of carrier approach guidance and recovery of land-based aircraft
|
Hernando, Jose-Luis
|
|
2016
|
|
5 |
p. 906-920
|
artikel
|
| 113 |
Quasi-continuous high-order sliding mode control-based fault-tolerant control for hypersonic flight vehicle via neural network observer
|
Cheng, Zian
|
|
2019
|
|
5 |
p. 1784-1800
|
artikel
|
| 114 |
Removal notice
|
|
|
|
|
5 |
p. NP3
|
artikel
|
| 115 |
Research and application of improved thin-layer element method of aero-engine bolted joints
|
Yao, Xingyu
|
|
2017
|
|
5 |
p. 823-839
|
artikel
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