| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Accessibility assessment and trajectory design for multiple Near-Earth-asteroids exploration using stand-alone CubeSats
|
Yu, Zhitong
|
|
|
118 |
C |
p.
|
artikel
|
| 2 |
A composite system theory-based guidance law for cooperative target circumnavigation of UAVs
|
Zhang, Min
|
|
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118 |
C |
p.
|
artikel
|
| 3 |
A 6-DOF sliding mode fault tolerant control solution for in-orbit autonomous rendezvous
|
Henry, David
|
|
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118 |
C |
p.
|
artikel
|
| 4 |
Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight
|
de Vries, Reynard
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|
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118 |
C |
p.
|
artikel
|
| 5 |
A hybrid particle swarm optimization-gauss pseudo method for reentry trajectory optimization of hypersonic vehicle with navigation information model
|
Wu, Yu
|
|
|
118 |
C |
p.
|
artikel
|
| 6 |
Analysis of the post-flutter aerothermoelastic characteristics of hypersonic skin panels using a CFD-based approach
|
Quan, Enqian
|
|
|
118 |
C |
p.
|
artikel
|
| 7 |
Analysis on stationary window of oblique detonation wave in methane-air mixture
|
Guo, Hongbo
|
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|
118 |
C |
p.
|
artikel
|
| 8 |
An efficient adjoint method for the aero-stealth shape optimization design
|
Li, Ming
|
|
|
118 |
C |
p.
|
artikel
|
| 9 |
An on-line deep learning framework for low-thrust trajectory optimisation
|
Xie, Ruida
|
|
|
118 |
C |
p.
|
artikel
|
| 10 |
An optimal steering law for sailing with solar and planetary radiation pressure
|
Barles, Anaïs
|
|
|
118 |
C |
p.
|
artikel
|
| 11 |
An optimization approach for improving the solar array output power of stratospheric aerostat
|
Jiang, Yi
|
|
|
118 |
C |
p.
|
artikel
|
| 12 |
A novel finite-time prescribed performance control scheme for spacecraft attitude tracking
|
Gao, Shihong
|
|
|
118 |
C |
p.
|
artikel
|
| 13 |
Approximation-free-based adaptive integral robust control with prescribed performance for unknown pure feedback system with disturbance
|
Zhu, Bin
|
|
|
118 |
C |
p.
|
artikel
|
| 14 |
Are nonfragile controllers always better than fragile controllers in attitude control performance of post-capture flexible spacecraft?
|
Liu, Chuang
|
|
|
118 |
C |
p.
|
artikel
|
| 15 |
A simultaneous use of a leading-edge fillet and a non-axisymmetrically contoured endwall in a turbine stage
|
Turgut, Özhan H.
|
|
|
118 |
C |
p.
|
artikel
|
| 16 |
Assessment of UAM and drone noise impact on the environment based on virtual flights
|
Bian, Haoyu
|
|
|
118 |
C |
p.
|
artikel
|
| 17 |
A switching-based state-scaling design for prescribed-time stabilization of nonholonomic systems with actuator dead-zones
|
Hou, Deheng
|
|
|
118 |
C |
p.
|
artikel
|
| 18 |
Back-propagation suppression study based on intake configuration optimization for an air-breathing pulse detonation engine
|
Wang, Zhiwu
|
|
|
118 |
C |
p.
|
artikel
|
| 19 |
Blow-off characteristics of a premixed methane/air flame response to acoustic disturbances in a longitudinal combustor
|
Sun, Yongchao
|
|
|
118 |
C |
p.
|
artikel
|
| 20 |
Buckling-driven mechanisms for twisting control in adaptive composite wings
|
Zhang, Jiayao
|
|
|
118 |
C |
p.
|
artikel
|
| 21 |
Catalyzed combustion of a nanofluid fuel droplet containing polydopamine-coated metastable intermixed composite n-Al/CuO
|
Gao, Yi
|
|
|
118 |
C |
p.
|
artikel
|
| 22 |
Combined applications of analytic methods for detection of combustion instability triggering
|
Luong, Hung Truyen
|
|
|
118 |
C |
p.
|
artikel
|
| 23 |
Combustion promotion and agglomeration reduction of the composite propellant using graphene
|
Liu, Lu
|
|
|
118 |
C |
p.
|
artikel
|
| 24 |
Control of the oscillations of shock train using boundary layer suction
|
Petha Sethuraman, Vignesh Ram
|
|
|
118 |
C |
p.
|
artikel
|
| 25 |
Design and analysis of a supersonic axisymmetric inlet based on controllable bleed slots
|
Yuan, Huacheng
|
|
|
118 |
C |
p.
|
artikel
|
| 26 |
Design and evaluation of a conical hypersonic vehicle with an overturned aerodynamic layout
|
Xiong, Bing
|
|
|
118 |
C |
p.
|
artikel
|
| 27 |
Design and mechanical property studies of 3D re-entrant lattice auxetic structure
|
Shen, Jianbang
|
|
|
118 |
C |
p.
|
artikel
|
| 28 |
Development and dynamics of a 2SPU+UPU+SP parallel rotor of helicopter
|
Lu, Yi
|
|
|
118 |
C |
p.
|
artikel
|
| 29 |
Dimensionality-reduction-based surrogate models for real-time design space exploration of a jet engine compressor blade
|
Bird, Gregory D.
|
|
|
118 |
C |
p.
|
artikel
|
| 30 |
Distributed optimal control allocation for 6-dof spacecraft with redundant thrusters
|
Lang, Xiaoyu
|
|
|
118 |
C |
p.
|
artikel
|
| 31 |
Editorial Board
|
|
|
|
118 |
C |
p.
|
artikel
|
| 32 |
Effect of a blade end slot on supersonic compressor cascade hub-corner separation
|
Ma, Jianci
|
|
|
118 |
C |
p.
|
artikel
|
| 33 |
Effect of poroelastic material on vibroacoustic behavior of truncated conical shells
|
Golzari, Masoud
|
|
|
118 |
C |
p.
|
artikel
|
| 34 |
Effects of acoustic liner on thermoacoustic instabilities in a premixed swirl combustor
|
Xu, Liangliang
|
|
|
118 |
C |
p.
|
artikel
|
| 35 |
Effects of wing kinematics, corrugation, and clap-and-fling on aerodynamic efficiency of a hovering insect-inspired flapping-wing micro air vehicle
|
Nguyen, Khanh
|
|
|
118 |
C |
p.
|
artikel
|
| 36 |
Enhancement of wake vortex decay by air blowing from the ground
|
Xu, Ziming
|
|
|
118 |
C |
p.
|
artikel
|
| 37 |
Error-constrained fixed-time trajectory tracking control for a stratospheric airship with disturbances
|
Yuan, Jiace
|
|
|
118 |
C |
p.
|
artikel
|
| 38 |
Experimental and numerical investigation on flame propagation and transition to detonation in curved channel
|
Pan, Zhenhua
|
|
|
118 |
C |
p.
|
artikel
|
| 39 |
Explainable Deep Reinforcement Learning for UAV autonomous path planning
|
He, Lei
|
|
|
118 |
C |
p.
|
artikel
|
| 40 |
Fractional-order resolved acceleration control for free-floating space manipulator with system uncertainty
|
Shao, Xiangyu
|
|
|
118 |
C |
p.
|
artikel
|
| 41 |
Free vibration analysis of rotating FG-CNT reinforced composite beams in thermal environments with general boundary conditions
|
Xu, Jiang
|
|
|
118 |
C |
p.
|
artikel
|
| 42 |
Fuzzy-based continuous current control of electrodynamic tethers for stable and efficient orbital boost
|
Liu, Jinyu
|
|
|
118 |
C |
p.
|
artikel
|
| 43 |
Generalized sail trajectory approximation with applications to MagSails
|
Bassetto, Marco
|
|
|
118 |
C |
p.
|
artikel
|
| 44 |
Hazardous flight region prediction for a small UAV operated in an urban area using a deep neural network
|
Jeong, Shinkyu
|
|
|
118 |
C |
p.
|
artikel
|
| 45 |
High-precision modeling and collision simulation of small rotor UAV
|
Zhang, Yongjie
|
|
|
118 |
C |
p.
|
artikel
|
| 46 |
Hybrid FWPS cooperation algorithm based unmanned aerial vehicle constrained path planning
|
Zhang, Xiangyin
|
|
|
118 |
C |
p.
|
artikel
|
| 47 |
Ignition dynamics and combustion mode transitions in a rocket-based combined cycle combustor operating in the ramjet/scramjet mode
|
An, Bin
|
|
|
118 |
C |
p.
|
artikel
|
| 48 |
Improved nonlinear MPC for aircraft gas turbine engine based on semi-alternative optimization strategy
|
Pang, Shuwei
|
|
|
118 |
C |
p.
|
artikel
|
| 49 |
Information sparsification for visual-inertial odometry by manipulating Bayes tree
|
Zhang, Xin
|
|
|
118 |
C |
p.
|
artikel
|
| 50 |
Integration of path planning, trajectory generation and trajectory tracking control for aircraft mission autonomy
|
Woo, Ji Won
|
|
|
118 |
C |
p.
|
artikel
|
| 51 |
Intelligent sensitivity analysis framework based on machine learning for spacecraft thermal design
|
Xiong, Yan
|
|
|
118 |
C |
p.
|
artikel
|
| 52 |
Investigation on film cooling and aerodynamic performance of blade tip with tangential jet cooling scheme at transonic flow
|
Zhang, Bo-lun
|
|
|
118 |
C |
p.
|
artikel
|
| 53 |
Investigation on the drag reduction and thermal protection properties of the porous opposing jet in the supersonic flow: A parametric study with constant mass flow rate
|
Ji, Chen
|
|
|
118 |
C |
p.
|
artikel
|
| 54 |
Iterative two-layer thermal design strategy for step sandwich antenna of space solar power satellite using modified constrained multi-objective optimization
|
Yang, Chen
|
|
|
118 |
C |
p.
|
artikel
|
| 55 |
Joint estimation of target location and relative altitude from angle measurements
|
Luo, Ji-An
|
|
|
118 |
C |
p.
|
artikel
|
| 56 |
Landmark database selection for vision-aided inertial navigation in planetary landing missions
|
Xu, Chao
|
|
|
118 |
C |
p.
|
artikel
|
| 57 |
Largest recoverable component based fault recoverability of UAV swarm with removal of faulty individuals
|
Peng, Yue
|
|
|
118 |
C |
p.
|
artikel
|
| 58 |
Lightweight implementation of natural vibration frequency adjustment of satellite structures by varying the structural stiffness
|
Guo, Jinsheng
|
|
|
118 |
C |
p.
|
artikel
|
| 59 |
Mission planning for Earth observation satellite with competitive learning strategy
|
Liu, Yuchen
|
|
|
118 |
C |
p.
|
artikel
|
| 60 |
Noise attenuation of quadrotor using phase synchronization method
|
Guan, Shujun
|
|
|
118 |
C |
p.
|
artikel
|
| 61 |
Numerical and experimental flight verifications of a calibration matrix approach for load monitoring and temperature reconstruction and compensation
|
Colombo, Luca
|
|
|
118 |
C |
p.
|
artikel
|
| 62 |
Numerical study on the induced-ramp mixed and combustion characteristics of rocket-based combined cycle engine
|
Jian, Dai
|
|
|
118 |
C |
p.
|
artikel
|
| 63 |
Online midcourse guidance method for boost phase interception via adaptive convex programming
|
Yang, Biao
|
|
|
118 |
C |
p.
|
artikel
|
| 64 |
On the effect of the correction of modelled airfoil tonal noise for a spanwise extension
|
du Plessis, Clarice
|
|
|
118 |
C |
p.
|
artikel
|
| 65 |
Panel flutter mechanism of rectangular solar sails based on traveling mode analysis
|
Liu, Zi-Xiao
|
|
|
118 |
C |
p.
|
artikel
|
| 66 |
Performance analysis and optimal sizing of electric multirotors
|
de Angelis, Emanuele L.
|
|
|
118 |
C |
p.
|
artikel
|
| 67 |
Piece-wise affine MPC-based attitude control for a CubeSat during orbital manoeuvres
|
Zhang, Xiaohua
|
|
|
118 |
C |
p.
|
artikel
|
| 68 |
Reinforcement learning vibration control for a flexible hinged plate
|
Qiu, Zhi-cheng
|
|
|
118 |
C |
p.
|
artikel
|
| 69 |
Research on the influence of integrated infrared suppressor exhaust angle on exhaust plume and helicopter infrared radiation
|
Yang, Zongyao
|
|
|
118 |
C |
p.
|
artikel
|
| 70 |
Review of designs and flight control techniques of hybrid and convertible VTOL UAVs
|
Ducard, Guillaume J.J.
|
|
|
118 |
C |
p.
|
artikel
|
| 71 |
Robust adaptive sliding mode attitude control for aircraft systems based on back-stepping method
|
Zhuang, Huixuan
|
|
|
118 |
C |
p.
|
artikel
|
| 72 |
Robust integrated covariance intersection fusion Kalman estimators for networked systems with a unified measurement model including five uncertainties
|
Ran, Chenjian
|
|
|
118 |
C |
p.
|
artikel
|
| 73 |
Robust parameter estimation with outlier-contaminated correlated measurements and applications to aerodynamic coefficient identification
|
Liu, Yuanyuan
|
|
|
118 |
C |
p.
|
artikel
|
| 74 |
Roles of recirculating bubble on the performance of centrifugal compressors
|
Lin, Yun
|
|
|
118 |
C |
p.
|
artikel
|
| 75 |
Simulation of airborne collision between a drone and an aircraft nose
|
Lu, Xiaohua
|
|
|
118 |
C |
p.
|
artikel
|
| 76 |
Sloshing reduced-order models for aeroelastic analyses of innovative aircraft configurations
|
Colella, Marta
|
|
|
118 |
C |
p.
|
artikel
|
| 77 |
Spectral analysis and modelling of the spray liquid injection in a Lean Direct Injection (LDI) gas turbine combustor through Eulerian-Lagrangian Large Eddy Simulations
|
Broatch, A.
|
|
|
118 |
C |
p.
|
artikel
|
| 78 |
Structural damping models for passive aeroelastic control
|
Eugeni, M.
|
|
|
118 |
C |
p.
|
artikel
|
| 79 |
Study on unsaturated shapes of helium ballonet of rigid airship during ascent process
|
Zhu, Qiang
|
|
|
118 |
C |
p.
|
artikel
|
| 80 |
The flow features of Transverse Jets In Supersonic Crossflow
|
Zhang, Ziao
|
|
|
118 |
C |
p.
|
artikel
|
| 81 |
The spatial-temporal evolution process of flow field generated by a pulsed-DC plasma actuator in quiescent air
|
Yang, Pengyu
|
|
|
118 |
C |
p.
|
artikel
|
| 82 |
Three-dimensional consensus algorithm for nonsingular distributed cooperative guidance strategy
|
Yang, Xiaoyan
|
|
|
118 |
C |
p.
|
artikel
|
| 83 |
Transient aeroelastic response of a rotor on a sea-based oil rig during engagement operations
|
Zhao, Jiachen
|
|
|
118 |
C |
p.
|
artikel
|
| 84 |
Transient investigation of nozzle erosion in a long-time working hybrid rocket motor
|
Tian, Hui
|
|
|
118 |
C |
p.
|
artikel
|
| 85 |
Twin-fuselage configuration for improving fuel efficiency of passenger aircraft
|
Ma, Yiyuan
|
|
|
118 |
C |
p.
|
artikel
|
| 86 |
Unilateral alignment transfer neural network for fault diagnosis of aircraft engine
|
Li, Bing
|
|
|
118 |
C |
p.
|
artikel
|
| 87 |
Unsteady flows of a highly loaded turbine blade with flat endwall and contoured endwall
|
Su, Xinrong
|
|
|
118 |
C |
p.
|
artikel
|
| 88 |
Validation and insight of a full-scale S-76 helicopter rotor using the Lattice-Boltzmann Method
|
van der Velden, W.C.P.
|
|
|
118 |
C |
p.
|
artikel
|
| 89 |
Validation of transition modeling techniques for a simplified fuselage configuration
|
Krimmelbein, Normann
|
|
|
118 |
C |
p.
|
artikel
|
| 90 |
Vibration control of a rotating hub-plate with enhanced active constrained layer damping treatment
|
Jiang, Fan
|
|
|
118 |
C |
p.
|
artikel
|
| 91 |
Vortex evolution and flame propagation driven by oblique shock wave in supersonic reactive mixing layer
|
Zhang, Dongdong
|
|
|
118 |
C |
p.
|
artikel
|
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