| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active control of a non-linear landing gear system having oleo pneumatic shock absorber using robust linear quadratic regulator approach
|
Yazici, Hakan
|
|
2018
|
|
13 |
p. 2397-2411
|
artikel
|
| 2 |
Active flow control of bi-stable asymmetric vortices on a slender body by alternating synthetic jets
|
Wang, Qite
|
|
2018
|
|
13 |
p. 2477-2488
|
artikel
|
| 3 |
Active manipulator motion planning for planetary landform awareness
|
Leng, Shu
|
|
2019
|
|
13 |
p. 5057-5071
|
artikel
|
| 4 |
Adaptive back-stepping sliding mode guidance laws with autopilot dynamics and acceleration saturation consideration
|
Geng, Sheng-Tao
|
|
2019
|
|
13 |
p. 4853-4863
|
artikel
|
| 5 |
Adaptive estimation of attitude and angular velocity of malfunctioned satellites for on-orbit servicing
|
Yu, Feng
|
|
2016
|
|
13 |
p. 2425-2446
|
artikel
|
| 6 |
A dual-system cooperative co-evolutionary algorithm for satellite equipment layout optimization
|
Cui, Feng-Zhe
|
|
2018
|
|
13 |
p. 2432-2457
|
artikel
|
| 7 |
Aerodynamic evaluation of an unmanned aerial vehicle with variable sweep and span
|
Gong, Cheng
|
|
2019
|
|
13 |
p. 4980-4997
|
artikel
|
| 8 |
Aerodynamic modeling of a flexible flapping-wing micro-air vehicle in the bond graph environment with the aim of assessing the lateral control power
|
Karimian, Saeed
|
|
2019
|
|
13 |
p. 4998-5015
|
artikel
|
| 9 |
Airfoil performance degradation by coupling effects of supercooled raindrop icing and heavy rainfall
|
Wu, Zhenlong
|
|
2017
|
|
13 |
p. 2384-2395
|
artikel
|
| 10 |
Airframe/intake–exhaust integration design of flying wing using a multi-bump strategy
|
Gan, Wenbiao
|
|
2017
|
|
13 |
p. 2396-2407
|
artikel
|
| 11 |
An analytical and experimental study of a hybrid rocket motor
|
Rezaei, Hadi
|
|
2014
|
|
13 |
p. 2475-2486
|
artikel
|
| 12 |
A new method for rapid shock loss evaluation and reduction for the optimization design of a supersonic compressor cascade
|
Liu, Baojie
|
|
2018
|
|
13 |
p. 2458-2476
|
artikel
|
| 13 |
A novel high precision inertial measurement scheme and its optimization method for high-speed rotating ammunition
|
Wu, Qingya
|
|
2014
|
|
13 |
p. 2553-2566
|
artikel
|
| 14 |
Auto-landing guidance for unmanned aerial vehicle with engine flame-out
|
Kim, Young-Sam
|
|
2019
|
|
13 |
p. 4864-4878
|
artikel
|
| 15 |
Buckling failure modes of one-dimensional lattice truss composite structures
|
Sui, Qianqian
|
|
2018
|
|
13 |
p. 2565-2583
|
artikel
|
| 16 |
Combustion characteristics in a supersonic combustor with ethylene injection upstream of dual parallel cavities
|
Zhong, Zhan
|
|
2016
|
|
13 |
p. 2515-2522
|
artikel
|
| 17 |
Composite material structure optimization design and aeroelastic analysis on forward swept wing
|
Rongrong, Xue
|
|
2019
|
|
13 |
p. 4679-4695
|
artikel
|
| 18 |
Computational fluid dynamics-based approach for low-order models of propelling nozzle performance
|
Al-Akam, Aws
|
|
2019
|
|
13 |
p. 4879-4894
|
artikel
|
| 19 |
Conceptual design and analysis of blended-wing-body aircraft
|
van Dommelen, Jorrit
|
|
2014
|
|
13 |
p. 2452-2474
|
artikel
|
| 20 |
Control of unmanned aerial vehicle formations using virtual structural approach and trajectory linearisation control method
|
Ogunbodede, Oladapo T
|
|
2016
|
|
13 |
p. 2409-2424
|
artikel
|
| 21 |
Coordinated control of fuel flow-rate for a high-temperature high-speed wind tunnel
|
Cai, Chaozhi
|
|
2016
|
|
13 |
p. 2504-2514
|
artikel
|
| 22 |
Coordinated robust control based on extended state observer of dual-arm space robot with closed chain for transferring a target
|
Cheng, Jing
|
|
2018
|
|
13 |
p. 2489-2498
|
artikel
|
| 23 |
Design, modeling, and simulation of an INS system using an asymmetric structure of six accelerometers and its error analysis in the ECEF frame
|
Ghasemzadeh, Vahid
|
|
2017
|
|
13 |
p. 2345-2361
|
artikel
|
| 24 |
Design of a conflict-detection air traffic control tool for the implementation of continuous climb operations: A case study at Palma TMA
|
Pérez-Castán, Javier A
|
|
2019
|
|
13 |
p. 4839-4852
|
artikel
|
| 25 |
Design of a measurement system for use in static balancing a two-axis gimbaled antenna
|
Yan, WX
|
|
2014
|
|
13 |
p. 2530-2541
|
artikel
|
| 26 |
Dynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regime
|
Zikmund, Pavel
|
|
2017
|
|
13 |
p. 2479-2486
|
artikel
|
| 27 |
Effects of rotational speed on the leakage behavior, temperature increase, and swirl development of labyrinth seal in a compressor stator well
|
Liu, Gaowen
|
|
2017
|
|
13 |
p. 2362-2374
|
artikel
|
| 28 |
Efficiency analysis of moving-magnet linear oscillating motor with dual-resonance for linear electro-hydrostatic actuator
|
Wang, Tianyi
|
|
2017
|
|
13 |
p. 2487-2501
|
artikel
|
| 29 |
Estimation of feasible materials and thermal conditions in a trapezoidal fin using genetic algorithm
|
Das, Ranjan
|
|
2016
|
|
13 |
p. 2356-2368
|
artikel
|
| 30 |
Experimental investigation on ignition enhancement of partially covered cavities in a supersonic flow
|
Cai, Zun
|
|
2016
|
|
13 |
p. 2535-2539
|
artikel
|
| 31 |
Extraction process of charged droplets in ultrasonic electric propulsion system: An experimental study
|
He, Weiguo
|
|
2019
|
|
13 |
p. 5016-5028
|
artikel
|
| 32 |
Fast trajectory tracking of electromagnetic satellite formation with actuator saturation
|
Huang, Xian-Lin
|
|
2016
|
|
13 |
p. 2463-2472
|
artikel
|
| 33 |
Feasibility investigation of large-scale model suspended by cable-driven parallel robot in hypersonic wind tunnel test
|
Wang, Xiaoguang
|
|
2017
|
|
13 |
p. 2375-2383
|
artikel
|
| 34 |
Flight phase and altitude-dependent geometrical vertical flight plan optimization minimizing the total number of vertical plan segments
|
Dancila, Bogdan Dumitru
|
|
2019
|
|
13 |
p. 4825-4838
|
artikel
|
| 35 |
Flow control for suppression of self-excited rolling oscillation at high angles of attack
|
Geng, Xi
|
|
2017
|
|
13 |
p. 2408-2422
|
artikel
|
| 36 |
Flow control with perpendicular acoustic forcing on NACA 2415 aerofoil at low Reynolds numbers
|
Açıkel, Halil Hakan
|
|
2016
|
|
13 |
p. 2447-2462
|
artikel
|
| 37 |
Flow visualization and mechanisms of three-electrode sliding discharge plasma actuator
|
Zheng, Borui
|
|
2019
|
|
13 |
p. 4788-4799
|
artikel
|
| 38 |
Fluid–structure interaction and flight dynamics analysis of parachute–payload system during uncontrolled airdrop process
|
Gao, Xinglong
|
|
2018
|
|
13 |
p. 2499-2512
|
artikel
|
| 39 |
Fractional-order sliding mode control for deployment of tethered spacecraft system
|
Ma, Zhiqiang
|
|
2019
|
|
13 |
p. 4721-4734
|
artikel
|
| 40 |
Functional verification and performance tests of an ultra-low shock non-explosive actuator for hold-down and release mechanisms for space applications
|
Morais, OMF
|
|
2014
|
|
13 |
p. 2487-2495
|
artikel
|
| 41 |
Generalized explicit guidance with optimal time-to-go and realistic final velocity
|
Mondal, Sabyasachi
|
|
2019
|
|
13 |
p. 4926-4942
|
artikel
|
| 42 |
Heterogeneous multi-unmanned aerial vehicle task planning: Simultaneous attacks on targets using the Pythagorean hodograph curve
|
Yan, Fei
|
|
2019
|
|
13 |
p. 4735-4749
|
artikel
|
| 43 |
High-resolution simulation and parametric research on helicopter rotor vortex flowfield with TAMI control in hover
|
Ye, Zhou
|
|
2018
|
|
13 |
p. 2513-2526
|
artikel
|
| 44 |
Influence of mistuning on aerodynamic damping of blade in transonic compressor
|
Yang, XD
|
|
2016
|
|
13 |
p. 2523-2534
|
artikel
|
| 45 |
Investigation of groove casing treatment in a transonic compressor at different speeds with control volume method
|
Zhou, Xiaoyong
|
|
2016
|
|
13 |
p. 2392-2408
|
artikel
|
| 46 |
Joint optimization of battery mass and flight trajectory for high-altitude solar-powered aircraft
|
Gao, Xian-Zhong
|
|
2014
|
|
13 |
p. 2439-2451
|
artikel
|
| 47 |
Mathematical modeling and characteristic analysis of scramjet buzz
|
Chang, Juntao
|
|
2014
|
|
13 |
p. 2542-2552
|
artikel
|
| 48 |
Measuring and solving real coning motion of spinning carriers
|
Zhang, Shuangbiao
|
|
2016
|
|
13 |
p. 2369-2378
|
artikel
|
| 49 |
Mechanism investigation of enhancing the stability of an axial flow rotor by blade angle slots
|
Zhang, Haoguang
|
|
2019
|
|
13 |
p. 4750-4764
|
artikel
|
| 50 |
Method for analyzing the effect of projectile impact on aircraft fuel tank inerting for survivability design
|
Pei, Yang
|
|
2016
|
|
13 |
p. 2345-2355
|
artikel
|
| 51 |
Missile longitudinal autopilot design using a generalized extended state observer-based mixed H2/H∞ control method
|
Dong, Yi
|
|
2019
|
|
13 |
p. 4704-4720
|
artikel
|
| 52 |
Model-based analysis of boundary layer ingestion effect on lateral-directional aerodynamics using differentiated boundary conditions
|
Zhang, Jing
|
|
2017
|
|
13 |
p. 2452-2463
|
artikel
|
| 53 |
Modeling, control design, and influence analysis of catapult-assisted take-off process for carrier-based aircrafts
|
Zhen, Ziyang
|
|
2018
|
|
13 |
p. 2527-2540
|
artikel
|
| 54 |
Modeling of a reaction control jet interacting with high-speed cross-flow in slip flow regime
|
Bhagat, Apurva
|
|
2019
|
|
13 |
p. 5029-5044
|
artikel
|
| 55 |
Model predictive orbit control of a Low Earth Orbit satellite using Gauss’s variational equations
|
Tavakoli, MM
|
|
2014
|
|
13 |
p. 2385-2398
|
artikel
|
| 56 |
Morphing wing optimization for steady level flight
|
Körpe, Durmuş S
|
|
2017
|
|
13 |
p. 2317-2330
|
artikel
|
| 57 |
Noise analysis of the turbojet and turbofan engine tests
|
Huang, Jingjing
|
|
2014
|
|
13 |
p. 2414-2423
|
artikel
|
| 58 |
Numerical and experimental investigation of the mean and turbulent characteristics of a wing-tip vortex in the near field
|
O’Regan, Micheál S
|
|
2014
|
|
13 |
p. 2516-2529
|
artikel
|
| 59 |
Numerical investigation on the weight, speed, and installation location effects on fuel tank separation trajectory
|
Dehghan, Mahnaz
|
|
2017
|
|
13 |
p. 2331-2344
|
artikel
|
| 60 |
Numerical simulation of ice accretion under mixed-phase conditions
|
Zhang, Lifen
|
|
2016
|
|
13 |
p. 2473-2483
|
artikel
|
| 61 |
Numerical simulation of SGT-600 gas turbine combustor, flow characteristics analysis, and sensitivity measurement with respect to the main fuel holes diameter
|
Aligoodarz, Mohammadreza
|
|
2016
|
|
13 |
p. 2379-2391
|
artikel
|
| 62 |
Numerical study on the shock vector control in a rectangular supersonic nozzle
|
Wu, Kexin
|
|
2019
|
|
13 |
p. 4943-4965
|
artikel
|
| 63 |
One-dimensional unsteady design method for pulsed detonation engine nozzles
|
Qiu, Hua
|
|
2014
|
|
13 |
p. 2496-2507
|
artikel
|
| 64 |
On the trade-off between minimum fuel burn and maximum time between overhaul for an intercooled aeroengine
|
Saatlou, E Najafi
|
|
2014
|
|
13 |
p. 2424-2438
|
artikel
|
| 65 |
Performance improvement of supersonic nozzles design using a high-temperature model
|
Hamaidia, Walid
|
|
2019
|
|
13 |
p. 4895-4910
|
artikel
|
| 66 |
Prediction of dynamic derivatives for air-breathing hypersonic vehicle using a harmonic balance method
|
Chai, Zhenxia
|
|
2019
|
|
13 |
p. 4966-4979
|
artikel
|
| 67 |
Pure-tension non-linear sliding mode control for deployment of tethered satellite system
|
Ma, Zhiqiang
|
|
2018
|
|
13 |
p. 2541-2551
|
artikel
|
| 68 |
Quadrotor aircraft intelligent system identification experiment design
|
Alabsi, Mohammed
|
|
2019
|
|
13 |
p. 4911-4925
|
artikel
|
| 69 |
Rapid ascent trajectory optimization for guided rockets via sequential convex programming
|
Zhang, Kai
|
|
2019
|
|
13 |
p. 4800-4809
|
artikel
|
| 70 |
Refined zigzag theory for vibration analysis of viscoelastic functionally graded carbon nanotube reinforced composite microplates integrated with piezoelectric layers
|
Ghorbanpour Arani, A
|
|
2017
|
|
13 |
p. 2464-2478
|
artikel
|
| 71 |
Reliability-based robust design for kinematic accuracy of a mechanism with axiomatic theory
|
Qui, Jiwei
|
|
2018
|
|
13 |
p. 2412-2423
|
artikel
|
| 72 |
Robust constraint backstepping control for high-performance aircraft with account of unsteady aerodynamic effects
|
Zhou, Chijun
|
|
2016
|
|
13 |
p. 2484-2503
|
artikel
|
| 73 |
Selecting stratospheric airship energy storage system using analytic hierarchy process and physical programming
|
Lixue, Zhang
|
|
2014
|
|
13 |
p. 2508-2515
|
artikel
|
| 74 |
Sensor placement and moving horizon state/parameter estimation for flexible hypersonic vehicles
|
Chen, Erkang
|
|
2019
|
|
13 |
p. 4765-4778
|
artikel
|
| 75 |
Stability assessment of an airflow distorted military engine’s FAN
|
Triantafyllou, T
|
|
2018
|
|
13 |
p. 2584-2592
|
artikel
|
| 76 |
Strictly-lower-convex-function-constructing disturbance observer based adaptive back stepping control for hypersonic flight vehicles
|
Zuo, Jingxing
|
|
2018
|
|
13 |
p. 2552-2564
|
artikel
|
| 77 |
Study on vortex shedding mode on the wake of horn/ridge ice contamination under high-Reynolds conditions
|
Hu, Shufan
|
|
2019
|
|
13 |
p. 5045-5056
|
artikel
|
| 78 |
Supersonic nonlinear flutter of cross-ply laminated shallow shells
|
Yazdi, Ali A
|
|
2019
|
|
13 |
p. 4696-4703
|
artikel
|
| 79 |
Thermally induced deformation of ultra-large truss support membrane structure
|
Wang, Jie
|
|
2017
|
|
13 |
p. 2502-2512
|
artikel
|
| 80 |
Thrust control strategy based on the minimum combustor inlet Mach number to enhance the overall performance of a scramjet engine
|
Ji, Zifei
|
|
2019
|
|
13 |
p. 4810-4824
|
artikel
|
| 81 |
Trajectory tracking control of hypersonic vehicle considering modeling uncertainty
|
Wang, Yuxiao
|
|
2019
|
|
13 |
p. 4779-4787
|
artikel
|
| 82 |
Uncommon exit arrangement effects in airplane emergency evacuation
|
Martínez-Val, R
|
|
2018
|
|
13 |
p. 2424-2431
|
artikel
|
| 83 |
Unsteady numerical investigation of two different corrugated airfoils
|
Ho, WH
|
|
2017
|
|
13 |
p. 2423-2437
|
artikel
|
| 84 |
Vision-aided terrain referenced navigation for unmanned aerial vehicles using ground features
|
Lee, Dongjin
|
|
2014
|
|
13 |
p. 2399-2413
|
artikel
|
| 85 |
Vortex flow and lift generation of a non-slender reverse delta wing
|
Lee, T
|
|
2017
|
|
13 |
p. 2438-2451
|
artikel
|
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