| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Adaptive collision-free formation control for under-actuated spacecraft
|
Liu, Xiaoping
|
|
|
79 |
C |
p. 223-232
|
artikel
|
| 2 |
Aerodynamic model-based robust adaptive control for close formation flight
|
Zhang, Qingrui
|
|
|
79 |
C |
p. 5-16
|
artikel
|
| 3 |
Analysis and experiment of a bio-inspired flyable micro flapping wing rotor
|
Guo, S.
|
|
|
79 |
C |
p. 506-517
|
artikel
|
| 4 |
An approach for estimating perpetual endurance of the stratospheric solar-powered platform
|
Li, Jun
|
|
|
79 |
C |
p. 118-130
|
artikel
|
| 5 |
A new efficient simulation method based on Bayes' theorem and importance sampling Markov chain simulation to estimate the failure-probability-based global sensitivity measure
|
Wang, Yanping
|
|
|
79 |
C |
p. 364-372
|
artikel
|
| 6 |
Angular momentum of free variable mass systems is partially conserved
|
Nanjangud, Angadh
|
|
|
79 |
C |
p. 1-4
|
artikel
|
| 7 |
A novel control scheme for quadrotor UAV based upon active disturbance rejection control
|
Zhang, Yong
|
|
|
79 |
C |
p. 601-609
|
artikel
|
| 8 |
A numerical method for the solution of supersonic streamwise vortex dynamics
|
Viganò, Davide
|
|
|
79 |
C |
p. 310-317
|
artikel
|
| 9 |
A study on adaptive vibration control and energy conversion of highly flexible multifunctional wings
|
Tsushima, Natsuki
|
|
|
79 |
C |
p. 297-309
|
artikel
|
| 10 |
Automatic Carrier Landing System multilayer parameter design based on Cauchy Mutation Pigeon-Inspired Optimization
|
Yang, Zhiyuan
|
|
|
79 |
C |
p. 518-530
|
artikel
|
| 11 |
Bending and buckling analysis of functionally graded annular microplate integrated with piezoelectric layers based on layerwise theory using DQM
|
Hajmohammad, Mohammad Hadi
|
|
|
79 |
C |
p. 679-688
|
artikel
|
| 12 |
Characteristics and model of the initial spray caused by an aircraft elastic tire rolling on the water-contaminated runway
|
Zhang, Yujia
|
|
|
79 |
C |
p. 610-624
|
artikel
|
| 13 |
Comparison of box-wing and conventional aircraft mission performance using multidisciplinary analysis and optimization
|
Andrews, Stephen A.
|
|
|
79 |
C |
p. 336-351
|
artikel
|
| 14 |
Computational investigations of water collection efficiency on blades in unsteady vortex flowfield of rotor
|
Chen, Xi
|
|
|
79 |
C |
p. 482-491
|
artikel
|
| 15 |
Cooperative guidance with multiple constraints using convex optimization
|
Jiang, Huan
|
|
|
79 |
C |
p. 426-440
|
artikel
|
| 16 |
Disturbance observer based control for spacecraft proximity operations with path constraint
|
Li, Qi
|
|
|
79 |
C |
p. 154-163
|
artikel
|
| 17 |
Dynamics of flexible multibody systems with variable-speed control moment gyroscopes
|
Feng, Xiao
|
|
|
79 |
C |
p. 554-569
|
artikel
|
| 18 |
Eco-efficiency assessment of manufacturing carbon fiber reinforced polymers (CFRP) in aerospace industry
|
Al-Lami, Ali
|
|
|
79 |
C |
p. 669-678
|
artikel
|
| 19 |
Editorial Board
|
|
|
|
79 |
C |
p. ii
|
artikel
|
| 20 |
Efficient coning algorithm design from a bilateral structure
|
Tang, Chuanye
|
|
|
79 |
C |
p. 48-57
|
artikel
|
| 21 |
Elastic buckling and free vibration analyses of porous-cellular plates with uniform and non-uniform porosity distributions
|
Thang, Pham Toan
|
|
|
79 |
C |
p. 278-287
|
artikel
|
| 22 |
Experimental exploration of inlet start process in continuously variable Mach number wind tunnel
|
Yu, Kaikai
|
|
|
79 |
C |
p. 75-84
|
artikel
|
| 23 |
Experimental investigation on gliding arc discharge plasma ignition and flame stabilization in scramjet combustor
|
Feng, Rong
|
|
|
79 |
C |
p. 145-153
|
artikel
|
| 24 |
Fast and coupled solution for cooperative mission planning of multiple heterogeneous unmanned aerial vehicles
|
Wu, Weinan
|
|
|
79 |
C |
p. 131-144
|
artikel
|
| 25 |
Feasible zone for planetary entry vehicles
|
Liang, Zixuan
|
|
|
79 |
C |
p. 459-467
|
artikel
|
| 26 |
Finite-time H ∞ adaptive attitude fault-tolerant control for reentry vehicle involving control delay
|
Gao, Mingzhou
|
|
|
79 |
C |
p. 246-254
|
artikel
|
| 27 |
Finite-time model-assisted active disturbance rejection control with a novel parameters optimizer for hypersonic reentry vehicle subject to multiple disturbances
|
Yu, Yue
|
|
|
79 |
C |
p. 588-600
|
artikel
|
| 28 |
Flow separation control over an airfoil using dual excitation of DBD plasma actuators
|
Ebrahimi, Abbas
|
|
|
79 |
C |
p. 658-668
|
artikel
|
| 29 |
Forced vibration analysis of the hard-coating blisk considering the strain-dependent manner of the hard-coating damper
|
Gao, Feng
|
|
|
79 |
C |
p. 187-198
|
artikel
|
| 30 |
Generalized error analysis of analytical coarse alignment formulations for stationary SINS
|
O. Silva, Felipe
|
|
|
79 |
C |
p. 500-505
|
artikel
|
| 31 |
Gust response stabilization for rigid aircraft with multi-control-effectors based on a novel integrated control scheme
|
Liu, Jinglong
|
|
|
79 |
C |
p. 625-635
|
artikel
|
| 32 |
High blade lift generation through short rotor–stator axial spacing in a tiny pump
|
Xu, Han
|
|
|
79 |
C |
p. 328-335
|
artikel
|
| 33 |
In-flight compound homing methodology of parafoil delivery systems under multiple constraints
|
Sun, Hao
|
|
|
79 |
C |
p. 85-104
|
artikel
|
| 34 |
Influence of high fidelity structural models on the predicted mass of aircraft wing using design optimization
|
Dababneh, Odeh
|
|
|
79 |
C |
p. 164-173
|
artikel
|
| 35 |
Integrated robust adaptive tracking control of non-cooperative fly-around mission subject to input saturation and full state constraints
|
Huang, Yi
|
|
|
79 |
C |
p. 233-245
|
artikel
|
| 36 |
Intermittent back-flash phenomenon of supersonic combustion in the staged-strut scramjet engine
|
Zhu, Shaohua
|
|
|
79 |
C |
p. 70-74
|
artikel
|
| 37 |
Loosely-displaced geostationary orbits with hybrid sail propulsion
|
Liu, Yuan
|
|
|
79 |
C |
p. 105-117
|
artikel
|
| 38 |
Mean flow compressibility effects in transonic turbulence modeling
|
Xu, Jinglei
|
|
|
79 |
C |
p. 492-499
|
artikel
|
| 39 |
Modeling and dynamics of a bare tape-shaped tethered satellite system
|
Yu, B.S.
|
|
|
79 |
C |
p. 288-296
|
artikel
|
| 40 |
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors
|
Andreini, Antonio
|
|
|
79 |
C |
p. 266-277
|
artikel
|
| 41 |
Multi-fidelity aerodynamic design trade-off exploration using point-by-point Pareto set identification
|
Amrit, Anand
|
|
|
79 |
C |
p. 399-412
|
artikel
|
| 42 |
Multi-objective optimisation of aircraft departure trajectories
|
Zhang, Mengying
|
|
|
79 |
C |
p. 37-47
|
artikel
|
| 43 |
Non-cooperative maneuvering spacecraft tracking via a variable structure estimator
|
Guang, Zhai
|
|
|
79 |
C |
p. 352-363
|
artikel
|
| 44 |
Nonlinear response and buckling analysis of eccentrically stiffened FGM toroidal shell segments in thermal environment
|
Vuong, Pham Minh
|
|
|
79 |
C |
p. 383-398
|
artikel
|
| 45 |
Numerical investigation on the assistant restarting method of variable geometry for high Mach number inlet
|
Liu, Yuan
|
|
|
79 |
C |
p. 647-657
|
artikel
|
| 46 |
Onboard mission allocation for multi-satellite system in limited communication environment
|
Zheng, Zixuan
|
|
|
79 |
C |
p. 174-186
|
artikel
|
| 47 |
On maximizing safety in stochastic aircraft trajectory planning with uncertain thunderstorm development
|
Hentzen, Daniel
|
|
|
79 |
C |
p. 543-553
|
artikel
|
| 48 |
Optimal morphing – augmented dynamic soaring maneuvers for unmanned air vehicle capable of span and sweep morphologies
|
Mir, Imran
|
|
|
79 |
C |
p. 17-36
|
artikel
|
| 49 |
Optimal reconfigurations between equilibria of two-craft electromagnetic formations along manifolds
|
Qi, Da-wei
|
|
|
79 |
C |
p. 531-542
|
artikel
|
| 50 |
Optimization of bounded low-thrust rendezvous with terminal constraints by interval analysis
|
Ma, Hongliang
|
|
|
79 |
C |
p. 58-69
|
artikel
|
| 51 |
Optimization of SD7003 airfoil performance using TBL and CBL at low Reynolds numbers
|
Kamari, Dj.
|
|
|
79 |
C |
p. 199-211
|
artikel
|
| 52 |
Optimum distributed wing shaping and control loads for highly flexible aircraft
|
Hammerton, Jared R.
|
|
|
79 |
C |
p. 255-265
|
artikel
|
| 53 |
Parameter estimation for optimal asteroid transfer trajectories using supervised machine learning
|
Shang, Haibin
|
|
|
79 |
C |
p. 570-579
|
artikel
|
| 54 |
Roll reversal phenomenon control in flight vehicles
|
Mirzaei, Mojtaba
|
|
|
79 |
C |
p. 413-425
|
artikel
|
| 55 |
Rotor blade shape reconstruction from strain measurements
|
Bernardini, Giovanni
|
|
|
79 |
C |
p. 580-587
|
artikel
|
| 56 |
Study on pyroshock propagation through plates with joints and washers
|
Lee, Juho
|
|
|
79 |
C |
p. 441-458
|
artikel
|
| 57 |
Substructure-based distributed collaborative probabilistic analysis method for low-cycle fatigue damage assessment of turbine blade–disk
|
Gao, Haifeng
|
|
|
79 |
C |
p. 636-646
|
artikel
|
| 58 |
The influences of the header geometry on hydrocarbon fuel flow distribution in compact parallel channels
|
Jiang, Yuguang
|
|
|
79 |
C |
p. 318-327
|
artikel
|
| 59 |
Unsteady behavior of oblique shock train and boundary layer interactions
|
Wang, Chengpeng
|
|
|
79 |
C |
p. 212-222
|
artikel
|
| 60 |
Wake energy analysis method applied to the Boxprop propeller concept
|
Capitao Patrao, Alexandre
|
|
|
79 |
C |
p. 689-700
|
artikel
|
| 61 |
Weakly nonlinear instability of viscoelastic planar sheets with initial varicose disturbances
|
Xie, Luo
|
|
|
79 |
C |
p. 373-382
|
artikel
|
| 62 |
Wing flexibility effects on the flight performance of an insect-like flapping-wing micro-air vehicle
|
Nguyen, Anh Tuan
|
|
|
79 |
C |
p. 468-481
|
artikel
|
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