| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A cancelling method based on Nth-order SSC algorithm for solving active cancellation problems
|
Yi, Mingxu
|
|
2017
|
71 |
C |
p. 264-271
|
artikel
|
| 2 |
Adaptive backstepping fast terminal sliding mode controller design for ducted fan engine of thrust-vectored aircraft
|
Fazeli Asl, Sayed Bagher
|
|
2017
|
71 |
C |
p. 521-529
|
artikel
|
| 3 |
Adaptive optimal gliding guidance independent of QEGC
|
Zhu, Jianwen
|
|
2017
|
71 |
C |
p. 373-381
|
artikel
|
| 4 |
Adaptive unscented Kalman filter based on maximum posterior and random weighting
|
Gao, Zhaohui
|
|
2017
|
71 |
C |
p. 12-24
|
artikel
|
| 5 |
A design approach of wide-speed-range vehicles based on the cone-derived theory
|
Zhang, Tian-tian
|
|
2017
|
71 |
C |
p. 42-51
|
artikel
|
| 6 |
Aircraft parameter estimation using Hybrid Neuro Fuzzy and Artificial Bee Colony optimization (HNFABC) algorithm
|
Ghosh Roy, Abhishek
|
|
2017
|
71 |
C |
p. 772-782
|
artikel
|
| 7 |
A mixed probabilistic–geometric strategy for UAV optimum flight path identification based on bit-coded basic manoeuvres
|
Blasi, Luciano
|
|
2017
|
71 |
C |
p. 1-11
|
artikel
|
| 8 |
A multi-source information fusion fault diagnosis for aviation hydraulic pump based on the new evidence similarity distance
|
Lu, Chuanqi
|
|
2017
|
71 |
C |
p. 392-401
|
artikel
|
| 9 |
Analysis of the crash of a transport aircraft and assessment of fuzzy-logic stall recovery
|
Lan, Chuan-Tau
|
|
2017
|
71 |
C |
p. 231-244
|
artikel
|
| 10 |
An approach to estimate aircraft touchdown attitudes and control inputs
|
Wu, P.
|
|
2017
|
71 |
C |
p. 201-213
|
artikel
|
| 11 |
An efficient multiple point selection study for mesh deformation using radial basis functions
|
Li, Ch.-N.
|
|
2017
|
71 |
C |
p. 580-591
|
artikel
|
| 12 |
An investigation on the effect of pitchwise endwall design in a turbine cascade at different incidence angles
|
Kiran, K.N.
|
|
2017
|
71 |
C |
p. 382-391
|
artikel
|
| 13 |
A prescribed performance control approach guaranteeing small overshoot for air-breathing hypersonic vehicles via neural approximation
|
Bu, Xiangwei
|
|
2017
|
71 |
C |
p. 485-498
|
artikel
|
| 14 |
A robust astro-inertial integrated navigation algorithm based on star-coordinate matching
|
Wang, Rong
|
|
2017
|
71 |
C |
p. 68-77
|
artikel
|
| 15 |
Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation
|
Qiao, Qiao
|
|
2017
|
71 |
C |
p. 62-67
|
artikel
|
| 16 |
Balancing the radar and long wavelength infrared signature properties in concept analysis of combat aircraft – A proof of concept
|
Marcus, Carina
|
|
2017
|
71 |
C |
p. 733-741
|
artikel
|
| 17 |
Characteristics of base pressure fluctuations of a typical missile configuration with a propulsive jet
|
Viji, M.
|
|
2017
|
71 |
C |
p. 695-705
|
artikel
|
| 18 |
Comprehensive preliminary sizing/resizing method for a fixed wing – VTOL electric UAV
|
Tyan, Maxim
|
|
2017
|
71 |
C |
p. 30-41
|
artikel
|
| 19 |
Conceptual design, performance and stability analysis of a 200 passengers Blended Wing Body aircraft
|
Ammar, Sami
|
|
2017
|
71 |
C |
p. 325-336
|
artikel
|
| 20 |
Coverage-based cooperative guidance strategy against highly maneuvering target
|
Su, Wenshan
|
|
2017
|
71 |
C |
p. 147-155
|
artikel
|
| 21 |
Deployment strategies for planar multi-tethered satellite formation
|
Zhai, Guang
|
|
2017
|
71 |
C |
p. 475-484
|
artikel
|
| 22 |
Design and analysis on three-dimensional scramjet nozzles with shape transition
|
Lv, Zheng
|
|
2017
|
71 |
C |
p. 189-200
|
artikel
|
| 23 |
Developing an optimal layout design of a satellite system by considering natural frequency and attitude control constraints
|
Fakoor, Mahdi
|
|
2017
|
71 |
C |
p. 172-188
|
artikel
|
| 24 |
Dual-filter transfer alignment for airborne distributed POS based on PVAM
|
Lu, Zhaoxing
|
|
2017
|
71 |
C |
p. 136-146
|
artikel
|
| 25 |
Dual reduced kernel extreme learning machine for aero-engine fault diagnosis
|
Lu, Feng
|
|
2017
|
71 |
C |
p. 742-750
|
artikel
|
| 26 |
Dynamic modelling of heat transfer in thermal-acoustic fatigue tests
|
Yu, Wenjun
|
|
2017
|
71 |
C |
p. 675-684
|
artikel
|
| 27 |
Dynamic stability of rolling missiles with angle-of-attack feedback three-loop autopilot considering parasitic effect
|
Tian, Song
|
|
2017
|
71 |
C |
p. 592-602
|
artikel
|
| 28 |
Editorial Board
|
|
|
2017
|
71 |
C |
p. IFC
|
artikel
|
| 29 |
Effect of elastic deformation on flight dynamics of projectiles with large slenderness ratio
|
Hua, RuHao
|
|
2017
|
71 |
C |
p. 347-359
|
artikel
|
| 30 |
Enhancement of quality of modal test results of an unmanned aerial vehicle wing by implementing a multi-objective genetic algorithm optimization
|
Pedramasl, Nima
|
|
2017
|
71 |
C |
p. 447-463
|
artikel
|
| 31 |
Entry trajectory generation without reversal of bank angle
|
He, Ruizhi
|
|
2017
|
71 |
C |
p. 627-635
|
artikel
|
| 32 |
Experimental analysis of hydrogen peroxide film-cooling method for nontoxic hypergolic thruster
|
Kang, Hongjae
|
|
2017
|
71 |
C |
p. 751-762
|
artikel
|
| 33 |
Experimental and numerical investigation of flight dynamics of a generic lambda wing configuration
|
Nelson, Dane M.
|
|
2017
|
71 |
C |
p. 706-724
|
artikel
|
| 34 |
Experimental testing for the influences of rotation and tip clearance on the labyrinth seal in a compressor stator well
|
Kong, Xiaozhi
|
|
2017
|
71 |
C |
p. 556-567
|
artikel
|
| 35 |
Finite-time formation control for multiple flight vehicles with accurate linearization model
|
Zhao, Enjiao
|
|
2017
|
71 |
C |
p. 90-98
|
artikel
|
| 36 |
Finite-time tracking control of hypersonic vehicle with input saturation
|
Sun, Jing-Guang
|
|
2017
|
71 |
C |
p. 272-284
|
artikel
|
| 37 |
Flow simulation and optimal shape design of N3-X hybrid wing body configuration using a body force method
|
Kim, Hyoungjin
|
|
2017
|
71 |
C |
p. 661-674
|
artikel
|
| 38 |
Inertia parameters identification for cellular space robot through interaction
|
Chang, Haitao
|
|
2017
|
71 |
C |
p. 464-474
|
artikel
|
| 39 |
Influences of shield ratio on the infrared signature of serpentine nozzle
|
Cheng, Wen
|
|
2017
|
71 |
C |
p. 299-311
|
artikel
|
| 40 |
Laboratory experiments of resident space object capture by a spacecraft–manipulator system
|
Virgili-Llop, Josep
|
|
2017
|
71 |
C |
p. 530-545
|
artikel
|
| 41 |
LQG based model predictive control for gust load alleviation
|
Liu, Xiang
|
|
2017
|
71 |
C |
p. 499-509
|
artikel
|
| 42 |
Monitoring multi-axial vibrations of flexible rockets using sensor-instrumented reference strain structures
|
Tsushima, Natsuki
|
|
2017
|
71 |
C |
p. 285-298
|
artikel
|
| 43 |
Multi-body separation simulation with an improved general mesh deformation method
|
Wang, Gang
|
|
2017
|
71 |
C |
p. 763-771
|
artikel
|
| 44 |
Multidisciplinary optimisation of single-stage sounding rockets using solid propulsion
|
Okninski, Adam
|
|
2017
|
71 |
C |
p. 412-419
|
artikel
|
| 45 |
Multi-objective optimization for re-entry spacecraft conceptual design using a free-form shape generator
|
Viviani, Antonio
|
|
2017
|
71 |
C |
p. 312-324
|
artikel
|
| 46 |
New approach to investigate nonlinear dynamic response and vibration of imperfect functionally graded carbon nanotube reinforced composite double curved shallow shells subjected to blast load and temperature
|
Nguyen, Dinh Duc
|
|
2017
|
71 |
C |
p. 360-372
|
artikel
|
| 47 |
Numerical simulation of vortex generators on a winglet control surface
|
Brüderlin, M.
|
|
2017
|
71 |
C |
p. 651-660
|
artikel
|
| 48 |
Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen–air mixtures
|
Fang, Yishen
|
|
2017
|
71 |
C |
p. 256-263
|
artikel
|
| 49 |
Nussbaum-based fuzzy adaptive nonlinear fault-tolerant control for hypersonic vehicles with diverse actuator faults
|
Hu, Chaofang
|
|
2017
|
71 |
C |
p. 432-440
|
artikel
|
| 50 |
On the thermo-structural response of a composite closeout in a regeneratively cooled thrust chamber
|
Ferraiuolo, M.
|
|
2017
|
71 |
C |
p. 402-411
|
artikel
|
| 51 |
On the utilisation of nonlinear plasticity models in military aircraft fatigue estimation: A preliminary comparison
|
Agius, Dylan
|
|
2017
|
71 |
C |
p. 25-29
|
artikel
|
| 52 |
Optimization of slot geometry in shock wave boundary layer interaction phenomenon by using CFD–ANN–GA cycle
|
Karbasizadeh, M.
|
|
2017
|
71 |
C |
p. 163-171
|
artikel
|
| 53 |
Origin of side-loads in a subscale truncated ideal contour nozzle
|
Verma, S.B.
|
|
2017
|
71 |
C |
p. 725-732
|
artikel
|
| 54 |
Parameter-robust linear quadratic Gaussian technique for multi-agent slung load transportation
|
Lee, Hae-In
|
|
2017
|
71 |
C |
p. 119-127
|
artikel
|
| 55 |
Parametric study on the drag and heat flux reduction mechanism of forward-facing cavity on a blunt body in supersonic flows
|
Huang, Wei
|
|
2017
|
71 |
C |
p. 619-626
|
artikel
|
| 56 |
Perched landing manoeuvres with a variable sweep wing UAV
|
Greatwood, Colin
|
|
2017
|
71 |
C |
p. 510-520
|
artikel
|
| 57 |
Performance evaluation and thermography of solid-propellant microthrusters with laser-based throttling
|
Isakari, Shota
|
|
2017
|
71 |
C |
p. 99-108
|
artikel
|
| 58 |
Preliminary integrated analysis for modeling and optimizing space stations at conceptual level
|
Wang, Kaiqiang
|
|
2017
|
71 |
C |
p. 420-431
|
artikel
|
| 59 |
Quantitative description of non-equilibrium turbulent phenomena in compressors
|
Fang, Le
|
|
2017
|
71 |
C |
p. 78-89
|
artikel
|
| 60 |
Retargeting extreme learning machines for classification and their applications to fault diagnosis of aircraft engine
|
Zhao, Yong-Ping
|
|
2017
|
71 |
C |
p. 603-618
|
artikel
|
| 61 |
Robust prescribed performance tracking control for free-floating space manipulators with kinematic and dynamic uncertainty
|
Zhou, Zhi-Gang
|
|
2017
|
71 |
C |
p. 568-579
|
artikel
|
| 62 |
Simple control of oxidizer flux for efficient extinction–reignition on a single-stage hybrid rocket
|
Chiba, Kazuhisa
|
|
2017
|
71 |
C |
p. 109-118
|
artikel
|
| 63 |
Spiral coning manoeuvre for in-orbit low thrust characterisation in CubeSats
|
Macario-Rojas, A.
|
|
2017
|
71 |
C |
p. 337-346
|
artikel
|
| 64 |
Stability of spinning missile with homing proportional guidance law
|
Hu, Xiao
|
|
2017
|
71 |
C |
p. 546-555
|
artikel
|
| 65 |
Structural reliability sensitivity analysis based on classification of model output
|
Xiao, Sinan
|
|
2017
|
71 |
C |
p. 52-61
|
artikel
|
| 66 |
Study on the effects of ionization seeds on pulse detonation characteristics
|
Lin, Ling
|
|
2017
|
71 |
C |
p. 128-135
|
artikel
|
| 67 |
Swing principle in tether-assisted return mission from an elliptical orbit
|
Aslanov, Vladimir S.
|
|
2017
|
71 |
C |
p. 156-162
|
artikel
|
| 68 |
Time-to-go estimation for terminal sliding mode based impact angle constrained guidance
|
Hou, Zhiwei
|
|
2017
|
71 |
C |
p. 685-694
|
artikel
|
| 69 |
Two-dimensional heliocentric dynamics approximation of an electric sail with fixed attitude
|
Niccolai, Lorenzo
|
|
2017
|
71 |
C |
p. 441-446
|
artikel
|
| 70 |
UGV-to-UAV cooperative ranging for robust navigation in GNSS-challenged environments
|
Sivaneri, Victor O.
|
|
2017
|
71 |
C |
p. 245-255
|
artikel
|
| 71 |
Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction
|
Chen, Xianjia
|
|
2017
|
71 |
C |
p. 214-230
|
artikel
|
| 72 |
Variable-fidelity aerodynamic analysis of lift fan type aircraft
|
Prasad, Rachit
|
|
2017
|
71 |
C |
p. 636-650
|
artikel
|
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