| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Adaptive control of hypersonic vehicles based on characteristic models with fuzzy neural network estimators
|
Chang, Yafei
|
|
2017
|
68 |
C |
p. 475-485
|
artikel
|
| 2 |
Aerodynamic shape optimization of a transonic fan by an adjoint-response surface method
|
Tang, Xiao
|
|
2017
|
68 |
C |
p. 26-36
|
artikel
|
| 3 |
A health evaluation method of multicopters modeled by Stochastic Hybrid System
|
Zhao, Zhiyao
|
|
2017
|
68 |
C |
p. 149-162
|
artikel
|
| 4 |
Aircraft engine health prognostics based on logistic regression with penalization regularization and state-space-based degradation framework
|
Yu, Jianbo
|
|
2017
|
68 |
C |
p. 345-361
|
artikel
|
| 5 |
Aircraft navigation based on differentiation–integration observer
|
Wang, Xinhua
|
|
2017
|
68 |
C |
p. 109-122
|
artikel
|
| 6 |
Aircraft stall phenomenon analysis using nonlinearity index theory
|
Tapolcai, Daniel P.
|
|
2017
|
68 |
C |
p. 288-298
|
artikel
|
| 7 |
An axiomatic/asymptotic evaluation of best theories for isotropic metallic and functionally graded plates employing non-polynomic functions
|
Candiotti, S.
|
|
2017
|
68 |
C |
p. 179-192
|
artikel
|
| 8 |
A new adaptive finite time nonlinear guidance law to intercept maneuvering targets
|
Behnamgol, Vahid
|
|
2017
|
68 |
C |
p. 416-421
|
artikel
|
| 9 |
A new Multi-position calibration method for gyroscope's drift coefficients on centrifuge
|
Wang, Shi-ming
|
|
2017
|
68 |
C |
p. 104-108
|
artikel
|
| 10 |
An optimization-based procedure for self-generation of Re-entry Vehicles shape
|
Viviani, Antonio
|
|
2017
|
68 |
C |
p. 123-134
|
artikel
|
| 11 |
A potential game approach to multiple UAV cooperative search and surveillance
|
Li, Pei
|
|
2017
|
68 |
C |
p. 403-415
|
artikel
|
| 12 |
A robust optimization approach for airport departure metering under uncertain taxi-out time predictions
|
Murça, Mayara Condé Rocha
|
|
2017
|
68 |
C |
p. 269-277
|
artikel
|
| 13 |
A study on the unsteady conjugate heat transfer of hot gas valve
|
Lee, Kyungwook
|
|
2017
|
68 |
C |
p. 362-369
|
artikel
|
| 14 |
CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 – Part 1
|
Bennett, C.J.
|
|
2017
|
68 |
C |
p. 561-576
|
artikel
|
| 15 |
CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 – Part 2
|
Bennett, C.J.
|
|
2017
|
68 |
C |
p. 577-587
|
artikel
|
| 16 |
Collision avoidance of Coulomb spacecraft formations using multi-mode hall thrusters
|
Wang, Ting
|
|
2017
|
68 |
C |
p. 261-268
|
artikel
|
| 17 |
Corrigendum to “Waypoint constrained guidance for entry vehicles” [Aerosp. Sci. Technol. 52 (2016) 52–61]
|
Liang, Zixuan
|
|
2017
|
68 |
C |
p. 287
|
artikel
|
| 18 |
Deployment analysis for space cable net structures with varying topologies and parameters
|
Nie, Rui
|
|
2017
|
68 |
C |
p. 1-10
|
artikel
|
| 19 |
Design and structural analysis of unique structures under an internal vacuum
|
Cranston, Brian
|
|
2017
|
68 |
C |
p. 68-76
|
artikel
|
| 20 |
3D grain burnback analysis using the partial interface tracking method
|
Ki, Wando
|
|
2017
|
68 |
C |
p. 58-67
|
artikel
|
| 21 |
Discrete event simulation of long-duration space station operations for rapid evaluation
|
Lin, Kun-Peng
|
|
2017
|
68 |
C |
p. 454-464
|
artikel
|
| 22 |
Dynamical modeling and multi-pulse chaotic dynamics of cantilevered pipe conveying pulsating fluid in parametric resonance
|
Zhang, Y.F.
|
|
2017
|
68 |
C |
p. 441-453
|
artikel
|
| 23 |
Dynamics of laminar separation bubble over NACA-0012 airfoil near stall conditions
|
AlMutairi, Jaber
|
|
2017
|
68 |
C |
p. 193-203
|
artikel
|
| 24 |
Editorial Board
|
|
|
2017
|
68 |
C |
p. IFC
|
artikel
|
| 25 |
Effective robust design of high lift NLF airfoil under multi-parameter uncertainty
|
Zhao, Huan
|
|
2017
|
68 |
C |
p. 530-542
|
artikel
|
| 26 |
Equilibrium configuration of a bounded inextensible membrane subject to solar radiation pressure
|
Fu, Bo
|
|
2017
|
68 |
C |
p. 552-560
|
artikel
|
| 27 |
Erratum to “Convective heat transfer and thermo-diffusion effects on flow of nanofluid towards a permeable stretching sheet saturated by a porous medium” [Aerospace Science and Technology 50 (2016) 196–203]
|
Khan, Umar
|
|
2017
|
68 |
C |
p. 588
|
artikel
|
| 28 |
Evaluation of free vibration and bending analysis of laminated composite and sandwich plates using non-polynomial zigzag models: C 0 Finite element formulation
|
Sarangan, Suganyadevi
|
|
2017
|
68 |
C |
p. 496-508
|
artikel
|
| 29 |
Extreme aircraft maneuver under sudden lateral CG movement: Modeling and control
|
Mukherjee, Bijoy K.
|
|
2017
|
68 |
C |
p. 11-25
|
artikel
|
| 30 |
Finite element modeling and pyroshock response analysis of separation nuts
|
Wang, Xixiong
|
|
2017
|
68 |
C |
p. 380-390
|
artikel
|
| 31 |
Improvement of Min–Max limit protection in aircraft engine control: An LMI approach
|
Imani, Amin
|
|
2017
|
68 |
C |
p. 214-222
|
artikel
|
| 32 |
Integral backstepping sliding mode control for quadrotor helicopter under external uncertain disturbances
|
Jia, Zhenyue
|
|
2017
|
68 |
C |
p. 299-307
|
artikel
|
| 33 |
Introduction of full flight dynamic stability constraints in aircraft multidisciplinary optimization
|
Mieloszyk, J.
|
|
2017
|
68 |
C |
p. 252-260
|
artikel
|
| 34 |
Inverse optical flow based guidance for UAV navigation through urban canyons
|
Agrawal, Pooja
|
|
2017
|
68 |
C |
p. 163-178
|
artikel
|
| 35 |
Limited memory optimal filter for discrete-time systems with measurement delay
|
Duan, Zhenhua
|
|
2017
|
68 |
C |
p. 422-430
|
artikel
|
| 36 |
Local and asymmetrical potential field approach to leader tracking problem in rigid formations of fixed-wing UAVs
|
Kownacki, Cezary
|
|
2017
|
68 |
C |
p. 465-474
|
artikel
|
| 37 |
Mixing augmentation induced by a vortex generator located upstream of the transverse gaseous jet in supersonic flows
|
Li, Lang-quan
|
|
2017
|
68 |
C |
p. 77-89
|
artikel
|
| 38 |
Numerical studies for performance improvement of a variable geometry dual mode combustor by optimizing deflection angle
|
Feng, Shuo
|
|
2017
|
68 |
C |
p. 320-330
|
artikel
|
| 39 |
Optimization of discrete cavities in a centrifugal compressor to enhance operating stability
|
Ma, Sang-Bum
|
|
2017
|
68 |
C |
p. 308-319
|
artikel
|
| 40 |
Pilot induced oscillation suppression controller design via nonlinear optimal output regulation method
|
Tran, Anh Tuan
|
|
2017
|
68 |
C |
p. 278-286
|
artikel
|
| 41 |
Pressure rising slope variation accompanying with combustion mode transition in a dual-mode combustor
|
Zhang, Chenlin
|
|
2017
|
68 |
C |
p. 370-379
|
artikel
|
| 42 |
Reduced basis methods for structurally nonlinear Joined Wings
|
Teunisse, Nick
|
|
2017
|
68 |
C |
p. 486-495
|
artikel
|
| 43 |
Regression rate characteristics of hybrid rocket motor with helical grain
|
Tian, Hui
|
|
2017
|
68 |
C |
p. 90-103
|
artikel
|
| 44 |
Reliability-based design optimization of rotating FGM cylindrical shells with temperature-dependent probabilistic frequency constraints
|
Safaeian Hamzehkolaei, Naser
|
|
2017
|
68 |
C |
p. 223-239
|
artikel
|
| 45 |
Research on centrifugal compressor disk containment of auxiliary power unit
|
Bai, Conger
|
|
2017
|
68 |
C |
p. 37-45
|
artikel
|
| 46 |
Robust finite time control algorithm for satellite attitude control
|
Li, You
|
|
2017
|
68 |
C |
p. 46-57
|
artikel
|
| 47 |
Robust weighted fusion Kalman estimators for systems with multiplicative noises, missing measurements and uncertain-variance linearly correlated white noises
|
Wang, Xuemei
|
|
2017
|
68 |
C |
p. 331-344
|
artikel
|
| 48 |
Separation control using quasi-radial wall jets
|
Javadi, Khodayar
|
|
2017
|
68 |
C |
p. 240-251
|
artikel
|
| 49 |
Solar sail trajectory analysis with asymptotic expansion method
|
Niccolai, Lorenzo
|
|
2017
|
68 |
C |
p. 431-440
|
artikel
|
| 50 |
Stabilization of rigid body attitude motion with time-delayed feedback
|
Samiei, Ehsan
|
|
2017
|
68 |
C |
p. 509-517
|
artikel
|
| 51 |
Static response and free vibration of functionally graded carbon nanotube-reinforced composite rectangular plates resting on Winkler–Pasternak elastic foundations
|
Duc, Nguyen Dinh
|
|
2017
|
68 |
C |
p. 391-402
|
artikel
|
| 52 |
Surrogate modeling for the main landing gear doors of an airbus passenger aircraft
|
Viúdez-Moreiras, D.
|
|
2017
|
68 |
C |
p. 135-148
|
artikel
|
| 53 |
Trustable UAV for higher level control architectures
|
Ashokkumar, Chimpalthradi R.
|
|
2017
|
68 |
C |
p. 204-213
|
artikel
|
| 54 |
Wing-body junction optimisation with CAD-based parametrisation including a moving intersection
|
Xu, Shenren
|
|
2017
|
68 |
C |
p. 543-551
|
artikel
|
| 55 |
Wing shape and dynamic twist design of bio-inspired nano air vehicles for forward flight purposes
|
Hassanalian, M.
|
|
2017
|
68 |
C |
p. 518-529
|
artikel
|
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