| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Adaptive nonlinear generalized predictive control for hypersonic vehicle with unknown parameters and control constraints
|
Tang, Tingting
|
|
2019
|
|
2 |
p. 510-532
|
artikel
|
| 2 |
Adaptive nonsingular terminal sliding mode cooperative guidance law in active defense scenario
|
Zou, Xinguang
|
|
2016
|
|
2 |
p. 307-320
|
artikel
|
| 3 |
Adaptive sliding mode backstepping control for attitude tracking of flexible spacecraft under input saturation and singularity
|
Xiao, B
|
|
2010
|
|
2 |
p. 199-214
|
artikel
|
| 4 |
Aerodynamic analysis and design of Busemann biplane: towards efficient supersonic flight
|
Maruyama, D
|
|
2012
|
|
2 |
p. 217-238
|
artikel
|
| 5 |
A global optimization control for turbo-fan engine acceleration schedule design
|
Zheng, Qiangang
|
|
2018
|
|
2 |
p. 308-316
|
artikel
|
| 6 |
A hierarchical decision and information system for multi-aircraft combat missions
|
Léchevin, N
|
|
2010
|
|
2 |
p. 133-148
|
artikel
|
| 7 |
Algorithm and operational concept for resolving short-range conflicts
|
Erzberger, H
|
|
2010
|
|
2 |
p. 225-243
|
artikel
|
| 8 |
Analysis of a mechanism with redundant drive for antenna pointing
|
Li, Xin
|
|
2017
|
|
2 |
p. 229-239
|
artikel
|
| 9 |
An approach to optimization of airport taxiway scheduling and traversal under uncertainty
|
Anderson, Ross
|
|
2013
|
|
2 |
p. 273-284
|
artikel
|
| 10 |
An automated multi-grid Chimera method based on the implicit hole technique
|
Liu, Qiuhong
|
|
2017
|
|
2 |
p. 279-293
|
artikel
|
| 11 |
A new approach for the linearization of dynamics in bolted joints
|
Khattak, Abdur R
|
|
2013
|
|
2 |
p. 226-234
|
artikel
|
| 12 |
An experimental investigation of transition point over a quasi-2D swept wing by using hot film
|
Khakmardani, Maryam Hassanzadeh
|
|
2015
|
|
2 |
p. 243-255
|
artikel
|
| 13 |
An experimental study of buffet detection on supercritical airfoils in transonic regime
|
Golestani, Ali
|
|
2015
|
|
2 |
p. 312-322
|
artikel
|
| 14 |
An extension of the streamline curvature through-flow design method for bypass fans of turbofan engines
|
Acarer, Sercan
|
|
2017
|
|
2 |
p. 240-253
|
artikel
|
| 15 |
A novel BeiDou weak signal acquisition scheme based on modified differential correlation
|
Han, Zhifeng
|
|
2019
|
|
2 |
p. 393-404
|
artikel
|
| 16 |
A novel prediction model for aircraft spare part intermittent demand in aviation transportation logistics using multi-components accumulation and high resolution analysis
|
Li, Zhixiong
|
|
2015
|
|
2 |
p. 384-395
|
artikel
|
| 17 |
An unsteady free wake model for aerodynamic performance of cycloidal propellers
|
Tang, Jiwei
|
|
2018
|
|
2 |
p. 290-307
|
artikel
|
| 18 |
A speech database for stress monitoring in the cockpit
|
Luig, Johannes
|
|
2014
|
|
2 |
p. 284-296
|
artikel
|
| 19 |
A three-dimensional numerical investigation on drag reduction of a supersonic spherical body with an opposing jet
|
Zhou, ChaoYing
|
|
2014
|
|
2 |
p. 163-177
|
artikel
|
| 20 |
A time suboptimal method for real-time spacecraft attitude agile maneuvering with angular velocity constraint
|
Wu, Yun-Hua
|
|
2019
|
|
2 |
p. 561-572
|
artikel
|
| 21 |
Attitude manoeuvre control and asymptotic disturbance rejection of flexible spacecraft
|
Yu, Zhen
|
|
2019
|
|
2 |
p. 426-437
|
artikel
|
| 22 |
Axiomatic design of a reflective multilayer high-temperature insulator
|
Torabi, Amin
|
|
2019
|
|
2 |
p. 457-471
|
artikel
|
| 23 |
Biobjective mission planning for geosynchronous satellites on-orbit refueling
|
Yu, Jing
|
|
2019
|
|
2 |
p. 686-697
|
artikel
|
| 24 |
Buckling/post-buckling strength of friction stir welded aircraft stiffened panels
|
Murphy, A
|
|
2014
|
|
2 |
p. 178-192
|
artikel
|
| 25 |
Collision avoidance maneuvers for multiple threatening objects using heuristic algorithms
|
Seong, Jae-Dong
|
|
2015
|
|
2 |
p. 256-268
|
artikel
|
| 26 |
Collision-free shape control of a plane tensegrity structure using an incremental dynamic relaxation method and a trial-and-error process
|
Xu, Xian
|
|
2013
|
|
2 |
p. 266-272
|
artikel
|
| 27 |
Computational analysis of vortices near casing in a transonic axial compressor rotor
|
Wu, Yanhui
|
|
2019
|
|
2 |
p. 710-724
|
artikel
|
| 28 |
Computational fluid dynamics investigation of finding appropriate location of fluidic anti-icing protective panel on leading edge of wing
|
Afghari, Mohammad Reza
|
|
2019
|
|
2 |
p. 698-709
|
artikel
|
| 29 |
Continuous time-varying sliding mode based attitude control for reentry vehicle
|
Wang, Liang
|
|
2015
|
|
2 |
p. 197-220
|
artikel
|
| 30 |
Cooperative path planning and task assignment for unmanned air vehicles
|
Innocenti, M
|
|
2010
|
|
2 |
p. 121-131
|
artikel
|
| 31 |
Co-operative unmanned aerial vehicle searching and mapping of complex obstacles using two-dimensional splinegon
|
Lazarus, S B
|
|
2010
|
|
2 |
p. 149-170
|
artikel
|
| 32 |
Coordinated formation control strategy of the rotating hub-spoke tethered formation system
|
Huang, Panfeng
|
|
2018
|
|
2 |
p. 317-330
|
artikel
|
| 33 |
Cost-range trade-off of intermediate stop operations of long-range transport airplanes
|
Martinez-Val, Rodrigo
|
|
2013
|
|
2 |
p. 394-404
|
artikel
|
| 34 |
Decentralized navigational state estimation for networked navigation systems with finite channel capacity and randomly switching topologies
|
Gao, Chao
|
|
2018
|
|
2 |
p. 201-214
|
artikel
|
| 35 |
Dependable Engines – The Story Of Pratt & Whitney
|
Newman, Simon
|
|
2012
|
|
2 |
p. 239-240
|
artikel
|
| 36 |
Design and comparison of autopilots of an air-to-surface antitank missile and its terminal guidance study
|
Ada, Celâl
|
|
2014
|
|
2 |
p. 193-205
|
artikel
|
| 37 |
Design of impact angle control guidance laws via high-performance sliding mode control
|
Lee, Chang-Hun
|
|
2013
|
|
2 |
p. 235-253
|
artikel
|
| 38 |
Design of liquid-propellant engine using collaborative optimization and evolutionary algorithms
|
Darabi, Hossein
|
|
2015
|
|
2 |
p. 232-242
|
artikel
|
| 39 |
Disturbance observer-based fault-tolerant attitude tracking control for rigid spacecraft with finite-time convergence
|
Zong, Qun
|
|
2019
|
|
2 |
p. 616-628
|
artikel
|
| 40 |
Disturbance-observer-based fixed-time second-order sliding mode control of an air-breathing hypersonic vehicle with actuator faults
|
Li, Peng
|
|
2018
|
|
2 |
p. 344-361
|
artikel
|
| 41 |
Dynamic characteristics of multifunctional structure for spacecraft
|
Hao, Dong
|
|
2019
|
|
2 |
p. 679-685
|
artikel
|
| 42 |
Effect of geometric parameters on the spray cone angle in the pressure swirl injector
|
Liu, Juan
|
|
2013
|
|
2 |
p. 342-353
|
artikel
|
| 43 |
Effect of oil droplet deformation on its deposited characteristics in an aeroengine bearing chamber
|
Chen, B
|
|
2014
|
|
2 |
p. 206-218
|
artikel
|
| 44 |
Elastic body impact on sandwich panels at low and intermediate velocity
|
Kralovec, Christoph
|
|
2015
|
|
2 |
p. 221-231
|
artikel
|
| 45 |
Experimental and three-dimensional numerical investigations on H2/air continuous rotating detonation wave
|
Liu, Shi-Jie
|
|
2013
|
|
2 |
p. 326-341
|
artikel
|
| 46 |
Experimental investigation on noise radiation characteristics of pulse detonation turbine engine
|
Huang, Xiqiao
|
|
2017
|
|
2 |
p. 254-264
|
artikel
|
| 47 |
Experimental research for flexible satellite dynamic simulation on three-axis air-bearing table
|
Liu, Yingying
|
|
2013
|
|
2 |
p. 369-380
|
artikel
|
| 48 |
Experimental studies on rotary valves for single-tube pulse detonation rocket engines
|
Wang, Ke
|
|
2014
|
|
2 |
p. 262-270
|
artikel
|
| 49 |
Exploring optimum power unit of propulsion system for high altitude airship
|
Chen, Shengqi
|
|
2015
|
|
2 |
p. 301-311
|
artikel
|
| 50 |
Finite-time attitude controller design via dual-loop control strategy
|
Yin, Chun W
|
|
2018
|
|
2 |
p. 215-226
|
artikel
|
| 51 |
Finite-time guidance laws for three-dimensional missile-target interception
|
Zhang, Zhenxing
|
|
2016
|
|
2 |
p. 392-403
|
artikel
|
| 52 |
Flap wise bending vibration and dynamic stability of rotating functionally graded material plates in thermal environments
|
Inala, Ramu
|
|
2017
|
|
2 |
p. 203-217
|
artikel
|
| 53 |
Frequency and damping identification in flutter flight testing using singular value decomposition and QR factorization
|
Barros-Rodríguez, José
|
|
2015
|
|
2 |
p. 323-332
|
artikel
|
| 54 |
Gas turbine performance monitoring based on extended information fusion filter
|
Lu, Feng
|
|
2019
|
|
2 |
p. 483-497
|
artikel
|
| 55 |
Guest Editorial
|
Gurfil, Pini
|
|
2010
|
|
2 |
p. i-ii
|
artikel
|
| 56 |
High performance direct torque control of electrical aerodynamics load simulator using adaptive fuzzy backstepping control
|
Ullah, Nasim
|
|
2015
|
|
2 |
p. 369-383
|
artikel
|
| 57 |
Impact of finite element idealisation on the prediction of welded fuselage stiffened panel buckling
|
Ekmekyapar, T
|
|
2016
|
|
2 |
p. 259-279
|
artikel
|
| 58 |
Improved Taylor analogy breakup and Clark models for droplet deformation prediction
|
Wu, Zhenlong
|
|
2019
|
|
2 |
p. 767-775
|
artikel
|
| 59 |
Input–output linearization minimum sliding-mode error feedback control for spacecraft formation with large perturbations
|
Cao, Lu
|
|
2015
|
|
2 |
p. 352-368
|
artikel
|
| 60 |
Internal flow and external jet characteristics of double serpentine nozzle with different aspect ratio
|
Xiao-lin, Sun
|
|
2019
|
|
2 |
p. 545-560
|
artikel
|
| 61 |
Introducing a novel algorithm for minimum-time low-thrust orbital transfers with free initial condition
|
Shafieenejad, I
|
|
2015
|
|
2 |
p. 333-351
|
artikel
|
| 62 |
Investigation of multiple-baseline stereovision for state estimation of unknown dynamic space targets
|
Jigalin, Anton
|
|
2016
|
|
2 |
p. 207-233
|
artikel
|
| 63 |
Investigation of particle size effect on flame velocity in the combustion of nano/micron-sized aluminum particles in air
|
Bidabadi, M
|
|
2014
|
|
2 |
p. 297-304
|
artikel
|
| 64 |
Investigation of the aerodynamic performance and flow physics on cross sections of Dragonfly wing on flapping and pitching motion in low Reynolds number
|
Lavimi, Roham
|
|
2019
|
|
2 |
p. 589-603
|
artikel
|
| 65 |
Lambert’s problem and solution by non-rational Bézier functions
|
Pan, Binfeng
|
|
2018
|
|
2 |
p. 227-245
|
artikel
|
| 66 |
Large amplitude flutter analysis of functionally graded carbon nanotube reinforced composite plates with piezoelectric layers on nonlinear elastic foundation
|
Yazdi, Ali A
|
|
2019
|
|
2 |
p. 533-544
|
artikel
|
| 67 |
Layout and configuration design for a satellite with variable mass using hybrid optimization method
|
Fakoor, M
|
|
2016
|
|
2 |
p. 360-377
|
artikel
|
| 68 |
Layout design optimization of a space propulsion system using hybrid optimization algorithm
|
Shafaee, Maziar
|
|
2017
|
|
2 |
p. 338-349
|
artikel
|
| 69 |
Matching suitability analysis for geomagnetic aided navigation based on an intelligent classification method
|
Wang, Peng
|
|
2014
|
|
2 |
p. 271-283
|
artikel
|
| 70 |
Mathematical modeling and linearized analysis of the jet-pipe hydraulic amplifier applied to a servovalve
|
Li, Yuesong
|
|
2019
|
|
2 |
p. 657-666
|
artikel
|
| 71 |
Meta-synthesis information fusion for hybrid diagnostics of space avionics
|
Xu, Jiuping
|
|
2014
|
|
2 |
p. 219-235
|
artikel
|
| 72 |
Micro-satellite angular rate estimation using second-order sliding mode observer
|
Pal, Madhumita
|
|
2016
|
|
2 |
p. 244-258
|
artikel
|
| 73 |
Mixed H∞/H2 gain-scheduled control for spacecraft rendezvous in elliptical orbits
|
Ma, Lichao
|
|
2014
|
|
2 |
p. 236-247
|
artikel
|
| 74 |
Modelling roughness effects for transitional low Reynolds number aerofoil flows
|
Liu, S
|
|
2015
|
|
2 |
p. 280-289
|
artikel
|
| 75 |
Modified Dubins parameterization for aircraft emergency trajectory planning
|
Yomchinda, Thanan
|
|
2017
|
|
2 |
p. 374-393
|
artikel
|
| 76 |
Modified unscented Kalman filter for X-ray pulsar-based navigation system in the presence of measurement outliers
|
Li, Xiaoyu
|
|
2018
|
|
2 |
p. 260-269
|
artikel
|
| 77 |
Multibody simulation of a generalized predictive controller for tiltrotor active aeroelastic control
|
Mattaboni, M
|
|
2012
|
|
2 |
p. 197-216
|
artikel
|
| 78 |
Multi-objective optimization procedure for the wing design at cruise and low-speed conditions
|
Bolsunovsky, Anatoly L
|
|
2013
|
|
2 |
p. 254-265
|
artikel
|
| 79 |
Multi-objective regulating and protecting control for ducted rocket using a bumpless transfer scheme
|
Bao, Wen
|
|
2013
|
|
2 |
p. 311-325
|
artikel
|
| 80 |
Multiple flight vehicles cooperative guidance law based on extended state observer and finite time consensus theory
|
Zhao, Enjiao
|
|
2018
|
|
2 |
p. 270-279
|
artikel
|
| 81 |
Natural motion of a multi-rotor aircraft
|
Ferrarese, Gastone
|
|
2018
|
|
2 |
p. 280-289
|
artikel
|
| 82 |
Neural network based optimal adaptive attitude control of near-space vehicle with system uncertainties and disturbances
|
Xia, Rongsheng
|
|
2019
|
|
2 |
p. 641-656
|
artikel
|
| 83 |
Nonlinear dynamic probabilistic design of turbine disk-radial deformation using extremum response surface method-based support vector machine of regression
|
Fei, Cheng-Wei
|
|
2015
|
|
2 |
p. 290-300
|
artikel
|
| 84 |
Nonlinear filtering techniques for geomagnetic navigation
|
Guo, Caifa
|
|
2014
|
|
2 |
p. 305-320
|
artikel
|
| 85 |
Numerical investigation of injection angle effects on shock vector control performance
|
Forghany, Farzad
|
|
2019
|
|
2 |
p. 405-417
|
artikel
|
| 86 |
Numerically and statistically stable Kalman filter for INS/GNSS integration
|
Liu, Ming
|
|
2016
|
|
2 |
p. 321-332
|
artikel
|
| 87 |
Numerical research on inlet total pressure distortion in a transonic compressor with non-axisymmetric stator
|
Sun, Peng
|
|
2019
|
|
2 |
p. 667-678
|
artikel
|
| 88 |
Numerical simulation of fairing separation test for hypersonic air breathing vehicle
|
Raj, Ankit
|
|
2017
|
|
2 |
p. 319-325
|
artikel
|
| 89 |
Numerical simulation of flow around a body of revolution with an appendage controlled by electromagnetic force
|
Liu, Huixing
|
|
2013
|
|
2 |
p. 303-310
|
artikel
|
| 90 |
Numerical simulation of parachute inflation: A methodological review
|
Cao, Yihua
|
|
2019
|
|
2 |
p. 736-766
|
artikel
|
| 91 |
Numerical study on the effect of geometrical parameters on the labyrinth–honeycomb seal performance
|
Alizadeh, Mohammad
|
|
2018
|
|
2 |
p. 362-373
|
artikel
|
| 92 |
On-line trajectory generation for autonomous unmanned vehicles in the presence of no-fly zones
|
De Lellis, Ettore
|
|
2013
|
|
2 |
p. 381-393
|
artikel
|
| 93 |
On–off and proportional–integral controller for a morphing wing. Part 1: Actuation mechanism and control design
|
Grigorie, T L
|
|
2012
|
|
2 |
p. 131-145
|
artikel
|
| 94 |
On–off and proportional–integral controller for a morphing wing. Part 2: Control validation – numerical simulations and experimental tests
|
Grigorie, T L
|
|
2012
|
|
2 |
p. 146-162
|
artikel
|
| 95 |
Optimal feedback stabilization of a two-axis gimbaled system subject to saturation nonlinearity and multiple disturbances
|
Zhan, ST
|
|
2014
|
|
2 |
p. 248-261
|
artikel
|
| 96 |
Orbital rendezvous mission planning with complex constraints
|
Yu, Jing
|
|
2016
|
|
2 |
p. 296-306
|
artikel
|
| 97 |
Performance characteristics and optimisation of a geared intercooled reversed flow core engine
|
Camilleri, William
|
|
2015
|
|
2 |
p. 269-279
|
artikel
|
| 98 |
Performance investigation of a pulse detonation turbine engine
|
Jie, Lu
|
|
2016
|
|
2 |
p. 350-359
|
artikel
|
| 99 |
Performance of a jaws inlet under off-design conditions
|
Gu, Tianlai
|
|
2017
|
|
2 |
p. 294-305
|
artikel
|
| 100 |
Planar periodic orbits’ construction around libration points with invariant manifold technique
|
Qian, Ying-Jing
|
|
2019
|
|
2 |
p. 498-509
|
artikel
|
| 101 |
Predictor-corrector guidance for entry vehicle based on fuzzy logic
|
Wang, Tao
|
|
2019
|
|
2 |
p. 472-482
|
artikel
|
| 102 |
Protection against overturning of a lunar-planetary lander using a controlled landing gear
|
Maeda, Takao
|
|
2019
|
|
2 |
p. 438-456
|
artikel
|
| 103 |
Reconfigurable flight control for robust transient response
|
Ashokkumar, Chimpalthradi R
|
|
2013
|
|
2 |
p. 405-411
|
artikel
|
| 104 |
Research on angles-only/SINS/CNS relative position and attitude determination algorithm for a tumbling spacecraft
|
Zhang, Lijun
|
|
2017
|
|
2 |
p. 218-228
|
artikel
|
| 105 |
Research on relative position and attitude representation and algorithm of formation flying systems based on position and attitude dual quaternion model
|
Zhu, Miao
|
|
2013
|
|
2 |
p. 354-368
|
artikel
|
| 106 |
Residual stress analysis of the multi-stage forging process of a nickel-based superalloy turbine disc
|
Ma, Yongjie
|
|
2013
|
|
2 |
p. 213-225
|
artikel
|
| 107 |
Robust adaptive finite-time attitude tracking and synchronization control for multi-spacecraft with actuator saturation
|
Zhu, Zhihao
|
|
2019
|
|
2 |
p. 629-640
|
artikel
|
| 108 |
Robust non-fragile state feedback attitude control for uncertain spacecraft with input saturation
|
Liu, Chuang
|
|
2018
|
|
2 |
p. 246-259
|
artikel
|
| 109 |
Role of information and communication in redefining unmanned aerial vehicle autonomous control levels
|
Suresh, M
|
|
2010
|
|
2 |
p. 171-197
|
artikel
|
| 110 |
Sensor fusions for constant thrust aircraft navigation in pitch plane
|
Ashokkumar, Chimpalthradi R
|
|
2018
|
|
2 |
p. 388-398
|
artikel
|
| 111 |
Shock wave propagation in non-uniform gas mixtures
|
Falcovitz, J
|
|
2012
|
|
2 |
p. 123-130
|
artikel
|
| 112 |
Sliding-mode-based contour-following controller for guidance and autopilot systems of launch vehicles
|
Yeh, Fu-Kuang
|
|
2013
|
|
2 |
p. 285-302
|
artikel
|
| 113 |
Sliding-mode control for staring-mode spacecraft using a disturbance observer
|
Wu, S N
|
|
2010
|
|
2 |
p. 215-224
|
artikel
|
| 114 |
Solar sail structural analysis via improved finite element modeling
|
Boni, Luisa
|
|
2017
|
|
2 |
p. 306-318
|
artikel
|
| 115 |
Stagnation pressure effect on Prandtl Meyer function for air
|
Salhi, Merouane
|
|
2017
|
|
2 |
p. 326-337
|
artikel
|
| 116 |
Study on flight safety manipulation space under complex conditions
|
Li, Zhe
|
|
2019
|
|
2 |
p. 725-735
|
artikel
|
| 117 |
Study on vibration of mistuned bladed disk with bi-periodic piezoelectric network
|
Deng, Peng-cheng
|
|
2017
|
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