| no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
| 1 |
A Bayesian network model integrated in a prognostics and health management system for aircraft line maintenance
|
Ferreiro, S
|
|
2011
|
|
8 |
p. 886-901
|
article
|
| 2 |
Adaptive finite time control for spacecraft attitude maneuver based on second-order terminal sliding mode
|
Ran, Dechao
|
|
2017
|
|
8 |
p. 1415-1427
|
article
|
| 3 |
Adaptive modeling of aircraft engine performance degradation model based on the equilibrium manifold and expansion form
|
Liu, Xiaofeng
|
|
2014
|
|
8 |
p. 1246-1272
|
article
|
| 4 |
A decentralized approach to formation flight routing of long-haul commercial flights
|
Verhagen, Collin MA
|
|
2019
|
|
8 |
p. 2992-3004
|
article
|
| 5 |
A fractional order proportional integral controller for path following and trajectory tracking of miniature air vehicles
|
Mand, Gagan Preet K
|
|
2014
|
|
8 |
p. 1389-1402
|
article
|
| 6 |
A method for deriving a non-singular state-space formulation based on Rubin's model for Pogo analysis
|
Tan, Shujun
|
|
2019
|
|
8 |
p. 2717-2730
|
article
|
| 7 |
Analysis of Strouhal number based equivalence of pitching and plunging airfoils and wake deflection
|
Khalid, Muhammad Saif Ullah
|
|
2015
|
|
8 |
p. 1423-1434
|
article
|
| 8 |
A new observer-based chattering-free sliding mode guidance law
|
Behnamgol, Vahid
|
|
2016
|
|
8 |
p. 1486-1495
|
article
|
| 9 |
An experimental and numerical investigation of the effect of geometric parameters on the flexible joint nonlinear behavior for thrust vector control
|
Ramezani, Mohammad Ali
|
|
2019
|
|
8 |
p. 2772-2782
|
article
|
| 10 |
ANFIS-Delta method for aerodynamic parameter estimation using flight data
|
Kumar, Ajit
|
|
2019
|
|
8 |
p. 3016-3032
|
article
|
| 11 |
Angular velocity estimation based on adaptive simplified spherical simplex unscented Kalman filter in GFSINS
|
Wu, Qingya
|
|
2014
|
|
8 |
p. 1375-1388
|
article
|
| 12 |
An internal model control-cascade Proportion-Integration-Differentiation method for manipulation of nano-quad-rotors
|
Wang, Yuan
|
|
2019
|
|
8 |
p. 2948-2955
|
article
|
| 13 |
An investigation into potential fuel savings for 110–130 seat passenger transport aircraft due to the incorporation of natural laminar flow or hybrid laminar flow control on the engine nacelles
|
Young, Trevor M
|
|
2013
|
|
8 |
p. 1300-1324
|
article
|
| 14 |
Attitude dynamics and thrust control for short tethered sub-satellite in deployment
|
Liu, Yingying
|
|
2015
|
|
8 |
p. 1407-1422
|
article
|
| 15 |
Automated conflict resolution, arrival management, and weather avoidance for air traffic management
|
Erzberger, H
|
|
2012
|
|
8 |
p. 930-949
|
article
|
| 16 |
Comparative investigation of tip leakage flow and its effect on stage performance in shrouded and unshrouded turbines
|
Gao, Jie
|
|
2013
|
|
8 |
p. 1265-1276
|
article
|
| 17 |
Comparative study of alternative biofuels on aircraft engine performance
|
Azami, Muhammad Hanafi
|
|
2017
|
|
8 |
p. 1509-1521
|
article
|
| 18 |
Comparison of linear models for gas turbine performance
|
Yu, Hu
|
|
2014
|
|
8 |
p. 1291-1301
|
article
|
| 19 |
Computational analysis of the effects of a boundary layer ingesting propulsion system in transonic flow
|
Mantič-Lugo, Vladislav
|
|
2013
|
|
8 |
p. 1215-1232
|
article
|
| 20 |
Computational fluid dynamics analysis of multi-element, high-lift aerofoil sections at transonic manoeuvre conditions
|
Johnston, LJ
|
|
2012
|
|
8 |
p. 912-929
|
article
|
| 21 |
Data-driven design paradigm in engineering problems
|
Liu, Changqing
|
|
2017
|
|
8 |
p. 1522-1534
|
article
|
| 22 |
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes
|
Xiao, Yabin
|
|
2016
|
|
8 |
p. 1496-1506
|
article
|
| 23 |
Design of top mounted supersonic inlets for a cylindrical fuselage
|
Saheby, Eiman B
|
|
2019
|
|
8 |
p. 2956-2979
|
article
|
| 24 |
Development of artificial dissipation schemes and compressible vorticity confinement methods
|
Bagheri-Esfeh, H
|
|
2011
|
|
8 |
p. 929-945
|
article
|
| 25 |
Development of a tool to study aircraft trajectory optimisation in the presence of icing conditions
|
Shinkafi, Ahmed
|
|
2015
|
|
8 |
p. 1464-1484
|
article
|
| 26 |
Development of a transonic wind tunnel to investigate engine bypass flow heat exchangers
|
Villafañe, L
|
|
2011
|
|
8 |
p. 902-914
|
article
|
| 27 |
Dynamically controlled variable-fidelity modelling for aircraft structural design optimisation
|
Allen, Jonathan G
|
|
2014
|
|
8 |
p. 1434-1449
|
article
|
| 28 |
Dynamical strength and design optimization of pipe-joint system under pressure impact load
|
Yongshou, L
|
|
2012
|
|
8 |
p. 1029-1040
|
article
|
| 29 |
Dynamic analysis and experimental verification of the carbon–carbon composite finger seal under complex working states
|
Wang, Li-Na
|
|
2019
|
|
8 |
p. 2914-2922
|
article
|
| 30 |
Dynamic control allocation for spacecraft attitude stabilization with actuator uncertainty
|
Zhang, Aihua
|
|
2014
|
|
8 |
p. 1336-1347
|
article
|
| 31 |
Dynamic separation minima coupled with wake vortex predictions in dependent runway configurations
|
Rad, T
|
|
2014
|
|
8 |
p. 1450-1457
|
article
|
| 32 |
Effect of interlayer slip on the damping of layered and welded aluminium beams
|
Singh, B
|
|
2012
|
|
8 |
p. 898-911
|
article
|
| 33 |
Effect of lip thickness on the aero-acoustic features of Hartmann whistle
|
Narayanan, S
|
|
2014
|
|
8 |
p. 1302-1313
|
article
|
| 34 |
Elliptic jet control with triangular tab
|
Aravindh Kumar, SM
|
|
2017
|
|
8 |
p. 1460-1477
|
article
|
| 35 |
Estimation of Simplified General Perturbations model 4 orbital elements from global positioning system data by invasive weed optimization algorithm
|
Bolandi, H
|
|
2015
|
|
8 |
p. 1384-1394
|
article
|
| 36 |
Evaluation of potential near-term operational changes to mitigate environmental impacts of aviation
|
Marais, Karen B
|
|
2013
|
|
8 |
p. 1277-1299
|
article
|
| 37 |
Experimental and numerical investigations of hole injection on the suction side throat of transonic turbine vanes in a cascade with trailing edge injection
|
Gao, Jie
|
|
2018
|
|
8 |
p. 1454-1466
|
article
|
| 38 |
Experimental investigation of propeller slipstream effects on the wing aerodynamics and boundary layer treatment at low Reynolds number
|
Aminaei, Hamzeh
|
|
2019
|
|
8 |
p. 3033-3041
|
article
|
| 39 |
Experimental investigation on the aerodynamic interaction between a helicopter and ground obstacles
|
Gibertini, G
|
|
2015
|
|
8 |
p. 1395-1406
|
article
|
| 40 |
Fault detection, isolation and accommodation for attitude control system of a three-axis satellite using interval linear parametric varying observers and fault tree analysis
|
Bolandi, Hossein
|
|
2014
|
|
8 |
p. 1403-1424
|
article
|
| 41 |
Finite-time output feedback control for the attitude of the spacecraft without unwinding
|
Guo, Yong
|
|
2018
|
|
8 |
p. 1421-1433
|
article
|
| 42 |
Flight dynamics and parametric modeling of a 2-DOF lab aircraft
|
Khan, Yasir Mahmood
|
|
2019
|
|
8 |
p. 2923-2931
|
article
|
| 43 |
Fractional differentiation-based observability analysis method for nonlinear X-ray pulsar navigation system
|
Liu, Jin
|
|
2018
|
|
8 |
p. 1467-1478
|
article
|
| 44 |
Geometrical approach-based defense-missile intercept guidance for aircraft protection against missile attack
|
Yamasaki, T
|
|
2012
|
|
8 |
p. 1014-1028
|
article
|
| 45 |
Grey-box modelling of a non-linear aerodynamic system using genetic algorithms
|
Rahideh, A
|
|
2011
|
|
8 |
p. 863-873
|
article
|
| 46 |
Ground experimental simulation method of infrared radiation of high altitude aircraft’s surface
|
Wang, Hao
|
|
2019
|
|
8 |
p. 2980-2991
|
article
|
| 47 |
Heat transfer effects and topology of the viscous interaction induced by surface protuberances in hypersonic flow
|
Haas, A
|
|
2012
|
|
8 |
p. 980-1001
|
article
|
| 48 |
Hybrid adaptive ascent flight control for a flexible launch vehicle
|
LeFevre, B D
|
|
2011
|
|
8 |
p. 851-862
|
article
|
| 49 |
Identification of pursued vehicles based on the guidance law recognition and line-of-sight analysis
|
Du, Runle
|
|
2019
|
|
8 |
p. 3005-3015
|
article
|
| 50 |
Impact-angle-constrained reentry guidance law guaranteeing convergence before attainment of desired line-of-sight range
|
Jiang, Chunwang
|
|
2019
|
|
8 |
p. 2783-2791
|
article
|
| 51 |
Indentation law for lightweight sandwich plates
|
Saadati, M
|
|
2011
|
|
8 |
p. 915-928
|
article
|
| 52 |
Innovative approach to air management strategy for turbocharged diesel aircraft engines
|
Katrašnik, T
|
|
2012
|
|
8 |
p. 966-979
|
article
|
| 53 |
Integrated improvement of the elasticity-based mesh deformation method based on robust parameters and mesh quality
|
Zhang, Bin
|
|
2019
|
|
8 |
p. 3078-3095
|
article
|
| 54 |
Integration of image de-blurring in an aerial Mono-SLAM
|
Atashgah, MA Amiri
|
|
2014
|
|
8 |
p. 1348-1362
|
article
|
| 55 |
Investigation of adding fins to external stores for improving the flutter characteristics of a wing/store configuration
|
Amoozgar, MR
|
|
2016
|
|
8 |
p. 1507-1517
|
article
|
| 56 |
Investigation of aerodynamic heating in V-shaped cowl-lip of the inward turning inlet
|
Meng, Zewei
|
|
2019
|
|
8 |
p. 2792-2801
|
article
|
| 57 |
Lightweight design for an aircraft reinforcing frame based on structural bionics
|
Xing, Denghai
|
|
2013
|
|
8 |
p. 1338-1346
|
article
|
| 58 |
Load relief control of launch vehicle using aerodynamic angle estimation
|
Oh, Gyeongtaek
|
|
2018
|
|
8 |
p. 1598-1605
|
article
|
| 59 |
Maximizing agility envelopes for reaction wheel spacecraft
|
Karpenko, Mark
|
|
2019
|
|
8 |
p. 2745-2759
|
article
|
| 60 |
Mechanical concept of W-WING whirl flutter aeroelastic demonstrator
|
Cecrdle, Jiri
|
|
2015
|
|
8 |
p. 1485-1494
|
article
|
| 61 |
Mechanical response of a panel section with a hexagonally tessellated stiffener grid
|
Bouazizi, M
|
|
2017
|
|
8 |
p. 1402-1414
|
article
|
| 62 |
MEMS gyroscope/TAM-integrated attitude estimation based on moving horizon estimation
|
Huang, Jingli
|
|
2017
|
|
8 |
p. 1451-1459
|
article
|
| 63 |
Micro air vehicle trajectory generation in pitch plane
|
Ashokkumar, Chimpalthradi R
|
|
2014
|
|
8 |
p. 1283-1290
|
article
|
| 64 |
Minimum time multiple-burn optimization of an upper stage with a finite thrust for satellite injection into geostationary orbit
|
Alavipour, Mojtaba
|
|
2018
|
|
8 |
p. 1542-1558
|
article
|
| 65 |
Missile acceleration controller design using proportional–integral and non-linear dynamic control design method
|
Kim, S-H
|
|
2012
|
|
8 |
p. 882-897
|
article
|
| 66 |
Modal parameter identification of structure under base excitation using vibration test data
|
Xia, JN
|
|
2017
|
|
8 |
p. 1428-1450
|
article
|
| 67 |
Multiobjective optimization for collision avoidance maneuver using a genetic algorithm
|
Seong, Jae-Dong
|
|
2016
|
|
8 |
p. 1438-1447
|
article
|
| 68 |
Multi-objective trade-off analysis of an integrated cold gas propulsion system
|
Banazadeh, Afshin
|
|
2013
|
|
8 |
p. 1233-1250
|
article
|
| 69 |
Multi-objective trajectory planning over terrain using label-setting greedy-based algorithm
|
Zardashti, R
|
|
2015
|
|
8 |
p. 1435-1453
|
article
|
| 70 |
Multiple failure prognosis of landing gear retraction/extension system based on H∞ filtering
|
Chen, Jie
|
|
2015
|
|
8 |
p. 1543-1555
|
article
|
| 71 |
New control methodology for a morphing wing demonstrator
|
Tchatchueng Kammegne, Michel Joël
|
|
2018
|
|
8 |
p. 1479-1494
|
article
|
| 72 |
Newton iterative method for potential flow problems based on variational principle and finite element type solution
|
Huang, Dian-Gui
|
|
2013
|
|
8 |
p. 1365-1371
|
article
|
| 73 |
Nonlinear adaptive sliding mode tracking control of an airplane with wing damage
|
Asadi, D
|
|
2018
|
|
8 |
p. 1405-1420
|
article
|
| 74 |
Nonlinear dynamic modeling in low frequency and control system stability domain determination for a LPE
|
Jafargholi, Ali
|
|
2016
|
|
8 |
p. 1467-1485
|
article
|
| 75 |
Novel acquisition of global positioning system signals based on parameter prediction and the chirp z-transform
|
Xu, Bing
|
|
2017
|
|
8 |
p. 1391-1401
|
article
|
| 76 |
Numerical investigation of flow upstream of a circular cylinder mounted vertically over a flat plate with gap
|
Khan, Ovais U
|
|
2015
|
|
8 |
p. 1531-1542
|
article
|
| 77 |
Numerical investigation of plasma actuated and non-actuated Gurney flaps on aerodynamic characteristics of a plunging airfoil
|
MahboubiDoust, A
|
|
2016
|
|
8 |
p. 1423-1437
|
article
|
| 78 |
Numerical investigation of the axial compressor performance with inlet distortions
|
Liu, ZX
|
|
2018
|
|
8 |
p. 1434-1441
|
article
|
| 79 |
Numerical modeling of adhesively bonded composite patch repair of cracked aluminum panels with concept of CZM and XFEM
|
Talebi, Behnam
|
|
2016
|
|
8 |
p. 1448-1466
|
article
|
| 80 |
Numerical modelling of a low Reynolds number plunging airfoil flow field characteristics
|
Amiralaei, Mohammad Reza
|
|
2013
|
|
8 |
p. 1251-1264
|
article
|
| 81 |
Numerical simulation of the airflow over a military aircraft with active intake
|
Triantafyllou, T
|
|
2017
|
|
8 |
p. 1369-1390
|
article
|
| 82 |
Numerical study of passive cavity control on high-pressure ratio single expansion ramp nozzle under over-expansion condition
|
Zhou, Li
|
|
2016
|
|
8 |
p. 1409-1422
|
article
|
| 83 |
Numerical study of the internal flow field of a dual pulse solid rocket motor including conjugate heat transfer
|
Li, Ying-kun
|
|
2017
|
|
8 |
p. 1535-1549
|
article
|
| 84 |
Numerical study on impulse characteristics of laser-supported air-breathing pulsed detonation thrusters
|
Li, Xiaokang
|
|
2014
|
|
8 |
p. 1324-1335
|
article
|
| 85 |
Oil damping energy loss analysis of landing gear shock absorber
|
Jiao, Fujun
|
|
2019
|
|
8 |
p. 3096-3106
|
article
|
| 86 |
Optimal impact angle control guidance law considering the seeker’s field-of-view limits
|
Park, Bong-Gyun
|
|
2013
|
|
8 |
p. 1347-1364
|
article
|
| 87 |
Optimal layout method of distributed locking device of satellite based on plant root growth theory
|
Wang, Gang
|
|
2019
|
|
8 |
p. 2802-2818
|
article
|
| 88 |
Optimisation of a 180° U-shaped bend shape for a turbine blade cooling passage leading to a pressure loss coefficient of approximately 0.6
|
Namgoong, Howoong
|
|
2016
|
|
8 |
p. 1371-1384
|
article
|
| 89 |
Optimization of the aerodynamic drag reduction of a passenger hatchback car
|
Guo, Ziyu
|
|
2019
|
|
8 |
p. 2819-2836
|
article
|
| 90 |
Orbit design and control method for satellite clusters and its applications to NetSat project
|
Zhou, Liang
|
|
2018
|
|
8 |
p. 1559-1570
|
article
|
| 91 |
Parametric reduced-order model approach for simulation and optimization of aeroelastic systems with structural nonlinearities
|
Castellani, Michele
|
|
2016
|
|
8 |
p. 1359-1370
|
article
|
| 92 |
Performance investigation of a supersonic air intake in the presence of the boundary layer suction
|
Soltani, MR
|
|
2015
|
|
8 |
p. 1495-1509
|
article
|
| 93 |
Pigeon-inspired optimization and lateral inhibition for image matching of autonomous aerial refueling
|
Sun, Yongbin
|
|
2018
|
|
8 |
p. 1571-1583
|
article
|
| 94 |
Pose measurement of nozzle based on laser range finders for capturing satellite
|
Zhang, Yu
|
|
2016
|
|
8 |
p. 1385-1396
|
article
|
| 95 |
Position control of linear electromechanical actuator for spoiler system base on the inverse system method
|
Cui, Yebing
|
|
2014
|
|
8 |
p. 1273-1282
|
article
|
| 96 |
Prediction of axial compressor blade excitation by using a two-way staggered fluid-structure interaction model
|
Brandsen, Jacobus D
|
|
2018
|
|
8 |
p. 1495-1514
|
article
|
| 97 |
Proper orthogonal decomposition analysis of boundary layer oscillating aspiration controlling separation flows in two-dimensional compressor cascades
|
Xu, Hao
|
|
2019
|
|
8 |
p. 2837-2852
|
article
|
| 98 |
Radar track segmentation with cubic splines for collision risk models in high density terminal areas
|
Cózar, JA
|
|
2015
|
|
8 |
p. 1371-1383
|
article
|
| 99 |
RBF neural network-based sliding mode vibration control of a flexible cantilever plate using laser displacement measurement
|
Qiu, Zhi-Cheng
|
|
2017
|
|
8 |
p. 1492-1508
|
article
|
| 100 |
Receding horizon control of a 3 DOF helicopter using online estimation of aerodynamic parameters
|
Mehndiratta, Mohit
|
|
2018
|
|
8 |
p. 1442-1453
|
article
|
| 101 |
Regeneratively cooled scramjet heat transfer calculation and comparison with experimental data
|
Jiang, Jin
|
|
2014
|
|
8 |
p. 1227-1234
|
article
|
| 102 |
Research of the suction flow control on wings at low Reynolds numbers
|
Ma, Dongli
|
|
2018
|
|
8 |
p. 1515-1528
|
article
|
| 103 |
Research on generalized inertial navigation system damping technology based on dual-model mean
|
Hongyang, He
|
|
2016
|
|
8 |
p. 1518-1527
|
article
|
| 104 |
Robust finite-time line-of-sight angular rate estimation in missile guidance
|
He, Shaoming
|
|
2017
|
|
8 |
p. 1550-1559
|
article
|
| 105 |
Side force over slender body with rings at different location at subsonic speed
|
Kumar, P
|
|
2017
|
|
8 |
p. 1478-1491
|
article
|
| 106 |
Simple model-free attitude control design for flexible spacecraft with prescribed performance
|
Zhang, Chao
|
|
2019
|
|
8 |
p. 2760-2771
|
article
|
| 107 |
Spacecraft attitude dynamics simulator actuated by cold gas propulsion system
|
Mirshams, Mehran
|
|
2015
|
|
8 |
p. 1510-1530
|
article
|
| 108 |
Spacecraft formation flying control under orbital perturbations by state-dependent Riccati equation method in the presence of on–off actuators
|
Rouzegar, Hossein
|
|
2019
|
|
8 |
p. 2853-2867
|
article
|
| 109 |
Statistical modelling for prediction of axis-switching in rectangular jets
|
Tipnis, Tanmay J
|
|
2013
|
|
8 |
p. 1325-1337
|
article
|
| 110 |
Supersonic viscous corner flows
|
Naidoo, P
|
|
2012
|
|
8 |
p. 950-965
|
article
|
| 111 |
The aerodynamic performance of a 2D lumped flexible airfoil in forward flight
|
Zhou, Chaoying
|
|
2014
|
|
8 |
p. 1363-1374
|
article
|
| 112 |
The design and performance evaluation of axial ventilator with honeycomb in the turbofan engine lubrication system
|
Jingyu, Zhao
|
|
2016
|
|
8 |
p. 1397-1408
|
article
|
| 113 |
The effect of different clearance geometry configurations on aerodynamic performance in a high-load compressor cascade
|
Chen, Shaowen
|
|
2014
|
|
8 |
p. 1425-1433
|
article
|
| 114 |
The GENUS aircraft conceptual design environment
|
Smith, H
|
|
2019
|
|
8 |
p. 2932-2947
|
article
|
| 115 |
The impact of circumferential casing grooves on rotating instability in a transonic axial compressor
|
Ye, Shubo
|
|
2019
|
|
8 |
p. 2868-2893
|
article
|
| 116 |
Theoretical investigation of the performance of alternative aviation fuels in an aero-engine combustion chamber
|
Uryga-Bugajska, I
|
|
2011
|
|
8 |
p. 874-885
|
article
|
| 117 |
Three-dimensional design and numerical simulation of magnetohydrodynamic controlled hypersonic inlets
|
Lu, H
|
|
2012
|
|
8 |
p. 1002-1013
|
article
|
| 118 |
Time accurate modelling of the secondary air system response to rapid transients
|
Gallar, L
|
|
2011
|
|
8 |
p. 946-958
|
article
|
| 119 |
Tolerance optimization by modification of Taguchi’s robust design approach and considering performance levels: Application to the design of a cold-expanded bushing
|
Paredes, Manuel
|
|
2014
|
|
8 |
p. 1314-1323
|
article
|
| 120 |
Tracking of spiraling reentry vehicles with varying frequency using a new target dynamic model
|
Ohlmeyer, Ernest J
|
|
2014
|
|
8 |
p. 1235-1245
|
article
|
| 121 |
Transitional flight equilibrium and performance study for the X-NMRL tail-sitter VTOL MAV
|
Tang, Wei
|
|
2019
|
|
8 |
p. 3056-3077
|
article
|
| 122 |
Two novel robust tracking control strategies for eliminating aircraft wing rock
|
Yin, Hang
|
|
2019
|
|
8 |
p. 3042-3055
|
article
|
| 123 |
Type-2 fuzzy adaptive sliding mode control of hypersonic flight
|
Jiao, Xin
|
|
2019
|
|
8 |
p. 2731-2744
|
article
|
| 124 |
Validation of an actuator disk model for numerical simulation of propeller
|
Li, Bo
|
|
2015
|
|
8 |
p. 1454-1463
|
article
|
| 125 |
Vibration and damping analysis of aerospace pipeline conveying fluid with constrained layer damping treatment
|
Gao, Pei-xin
|
|
2018
|
|
8 |
p. 1529-1541
|
article
|
| 126 |
Vision-based guidance for fixed-wing unmanned aerial vehicle autonomous carrier landing
|
Zhang, Zhouyu
|
|
2019
|
|
8 |
p. 2894-2913
|
article
|
| 127 |
Vision-based terrain referenced navigation of aerial vehicles using an adaptive extended Kalman filter
|
Mok, Sung-Hoon
|
|
2018
|
|
8 |
p. 1584-1597
|
article
|
Journal description