nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('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 |
artikel |
2 |
Adaptive finite time control for spacecraft attitude maneuver based on second-order terminal sliding mode
|
Ran, Dechao |
|
2017 |
|
8 |
p. 1415-1427 |
artikel |
3 |
Adaptive modeling of aircraft engine performance degradation model based on the equilibrium manifold and expansion form
|
Liu, Xiaofeng |
|
2014 |
|
8 |
p. 1246-1272 |
artikel |
4 |
A decentralized approach to formation flight routing of long-haul commercial flights
|
Verhagen, Collin MA |
|
2019 |
|
8 |
p. 2992-3004 |
artikel |
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 |
artikel |
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 |
artikel |
7 |
Analysis of Strouhal number based equivalence of pitching and plunging airfoils and wake deflection
|
Khalid, Muhammad Saif Ullah |
|
2015 |
|
8 |
p. 1423-1434 |
artikel |
8 |
A new observer-based chattering-free sliding mode guidance law
|
Behnamgol, Vahid |
|
2016 |
|
8 |
p. 1486-1495 |
artikel |
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 |
artikel |
10 |
ANFIS-Delta method for aerodynamic parameter estimation using flight data
|
Kumar, Ajit |
|
2019 |
|
8 |
p. 3016-3032 |
artikel |
11 |
Angular velocity estimation based on adaptive simplified spherical simplex unscented Kalman filter in GFSINS
|
Wu, Qingya |
|
2014 |
|
8 |
p. 1375-1388 |
artikel |
12 |
An internal model control-cascade Proportion-Integration-Differentiation method for manipulation of nano-quad-rotors
|
Wang, Yuan |
|
2019 |
|
8 |
p. 2948-2955 |
artikel |
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 |
artikel |
14 |
Attitude dynamics and thrust control for short tethered sub-satellite in deployment
|
Liu, Yingying |
|
2015 |
|
8 |
p. 1407-1422 |
artikel |
15 |
Automated conflict resolution, arrival management, and weather avoidance for air traffic management
|
Erzberger, H |
|
2012 |
|
8 |
p. 930-949 |
artikel |
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 |
artikel |
17 |
Comparative study of alternative biofuels on aircraft engine performance
|
Azami, Muhammad Hanafi |
|
2017 |
|
8 |
p. 1509-1521 |
artikel |
18 |
Comparison of linear models for gas turbine performance
|
Yu, Hu |
|
2014 |
|
8 |
p. 1291-1301 |
artikel |
19 |
Computational analysis of the effects of a boundary layer ingesting propulsion system in transonic flow
|
Mantič-Lugo, Vladislav |
|
2013 |
|
8 |
p. 1215-1232 |
artikel |
20 |
Computational fluid dynamics analysis of multi-element, high-lift aerofoil sections at transonic manoeuvre conditions
|
Johnston, LJ |
|
2012 |
|
8 |
p. 912-929 |
artikel |
21 |
Data-driven design paradigm in engineering problems
|
Liu, Changqing |
|
2017 |
|
8 |
p. 1522-1534 |
artikel |
22 |
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes
|
Xiao, Yabin |
|
2016 |
|
8 |
p. 1496-1506 |
artikel |
23 |
Design of top mounted supersonic inlets for a cylindrical fuselage
|
Saheby, Eiman B |
|
2019 |
|
8 |
p. 2956-2979 |
artikel |
24 |
Development of artificial dissipation schemes and compressible vorticity confinement methods
|
Bagheri-Esfeh, H |
|
2011 |
|
8 |
p. 929-945 |
artikel |
25 |
Development of a tool to study aircraft trajectory optimisation in the presence of icing conditions
|
Shinkafi, Ahmed |
|
2015 |
|
8 |
p. 1464-1484 |
artikel |
26 |
Development of a transonic wind tunnel to investigate engine bypass flow heat exchangers
|
Villafañe, L |
|
2011 |
|
8 |
p. 902-914 |
artikel |
27 |
Dynamically controlled variable-fidelity modelling for aircraft structural design optimisation
|
Allen, Jonathan G |
|
2014 |
|
8 |
p. 1434-1449 |
artikel |
28 |
Dynamical strength and design optimization of pipe-joint system under pressure impact load
|
Yongshou, L |
|
2012 |
|
8 |
p. 1029-1040 |
artikel |
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 |
artikel |
30 |
Dynamic control allocation for spacecraft attitude stabilization with actuator uncertainty
|
Zhang, Aihua |
|
2014 |
|
8 |
p. 1336-1347 |
artikel |
31 |
Dynamic separation minima coupled with wake vortex predictions in dependent runway configurations
|
Rad, T |
|
2014 |
|
8 |
p. 1450-1457 |
artikel |
32 |
Effect of interlayer slip on the damping of layered and welded aluminium beams
|
Singh, B |
|
2012 |
|
8 |
p. 898-911 |
artikel |
33 |
Effect of lip thickness on the aero-acoustic features of Hartmann whistle
|
Narayanan, S |
|
2014 |
|
8 |
p. 1302-1313 |
artikel |
34 |
Elliptic jet control with triangular tab
|
Aravindh Kumar, SM |
|
2017 |
|
8 |
p. 1460-1477 |
artikel |
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 |
artikel |
36 |
Evaluation of potential near-term operational changes to mitigate environmental impacts of aviation
|
Marais, Karen B |
|
2013 |
|
8 |
p. 1277-1299 |
artikel |
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 |
artikel |
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 |
artikel |
39 |
Experimental investigation on the aerodynamic interaction between a helicopter and ground obstacles
|
Gibertini, G |
|
2015 |
|
8 |
p. 1395-1406 |
artikel |
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 |
artikel |
41 |
Finite-time output feedback control for the attitude of the spacecraft without unwinding
|
Guo, Yong |
|
2018 |
|
8 |
p. 1421-1433 |
artikel |
42 |
Flight dynamics and parametric modeling of a 2-DOF lab aircraft
|
Khan, Yasir Mahmood |
|
2019 |
|
8 |
p. 2923-2931 |
artikel |
43 |
Fractional differentiation-based observability analysis method for nonlinear X-ray pulsar navigation system
|
Liu, Jin |
|
2018 |
|
8 |
p. 1467-1478 |
artikel |
44 |
Geometrical approach-based defense-missile intercept guidance for aircraft protection against missile attack
|
Yamasaki, T |
|
2012 |
|
8 |
p. 1014-1028 |
artikel |
45 |
Grey-box modelling of a non-linear aerodynamic system using genetic algorithms
|
Rahideh, A |
|
2011 |
|
8 |
p. 863-873 |
artikel |
46 |
Ground experimental simulation method of infrared radiation of high altitude aircraft’s surface
|
Wang, Hao |
|
2019 |
|
8 |
p. 2980-2991 |
artikel |
47 |
Heat transfer effects and topology of the viscous interaction induced by surface protuberances in hypersonic flow
|
Haas, A |
|
2012 |
|
8 |
p. 980-1001 |
artikel |
48 |
Hybrid adaptive ascent flight control for a flexible launch vehicle
|
LeFevre, B D |
|
2011 |
|
8 |
p. 851-862 |
artikel |
49 |
Identification of pursued vehicles based on the guidance law recognition and line-of-sight analysis
|
Du, Runle |
|
2019 |
|
8 |
p. 3005-3015 |
artikel |
50 |
Impact-angle-constrained reentry guidance law guaranteeing convergence before attainment of desired line-of-sight range
|
Jiang, Chunwang |
|
2019 |
|
8 |
p. 2783-2791 |
artikel |
51 |
Indentation law for lightweight sandwich plates
|
Saadati, M |
|
2011 |
|
8 |
p. 915-928 |
artikel |
52 |
Innovative approach to air management strategy for turbocharged diesel aircraft engines
|
Katrašnik, T |
|
2012 |
|
8 |
p. 966-979 |
artikel |
53 |
Integrated improvement of the elasticity-based mesh deformation method based on robust parameters and mesh quality
|
Zhang, Bin |
|
2019 |
|
8 |
p. 3078-3095 |
artikel |
54 |
Integration of image de-blurring in an aerial Mono-SLAM
|
Atashgah, MA Amiri |
|
2014 |
|
8 |
p. 1348-1362 |
artikel |
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 |
artikel |
56 |
Investigation of aerodynamic heating in V-shaped cowl-lip of the inward turning inlet
|
Meng, Zewei |
|
2019 |
|
8 |
p. 2792-2801 |
artikel |
57 |
Lightweight design for an aircraft reinforcing frame based on structural bionics
|
Xing, Denghai |
|
2013 |
|
8 |
p. 1338-1346 |
artikel |
58 |
Load relief control of launch vehicle using aerodynamic angle estimation
|
Oh, Gyeongtaek |
|
2018 |
|
8 |
p. 1598-1605 |
artikel |
59 |
Maximizing agility envelopes for reaction wheel spacecraft
|
Karpenko, Mark |
|
2019 |
|
8 |
p. 2745-2759 |
artikel |
60 |
Mechanical concept of W-WING whirl flutter aeroelastic demonstrator
|
Cecrdle, Jiri |
|
2015 |
|
8 |
p. 1485-1494 |
artikel |
61 |
Mechanical response of a panel section with a hexagonally tessellated stiffener grid
|
Bouazizi, M |
|
2017 |
|
8 |
p. 1402-1414 |
artikel |
62 |
MEMS gyroscope/TAM-integrated attitude estimation based on moving horizon estimation
|
Huang, Jingli |
|
2017 |
|
8 |
p. 1451-1459 |
artikel |
63 |
Micro air vehicle trajectory generation in pitch plane
|
Ashokkumar, Chimpalthradi R |
|
2014 |
|
8 |
p. 1283-1290 |
artikel |
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 |
artikel |
65 |
Missile acceleration controller design using proportional–integral and non-linear dynamic control design method
|
Kim, S-H |
|
2012 |
|
8 |
p. 882-897 |
artikel |
66 |
Modal parameter identification of structure under base excitation using vibration test data
|
Xia, JN |
|
2017 |
|
8 |
p. 1428-1450 |
artikel |
67 |
Multiobjective optimization for collision avoidance maneuver using a genetic algorithm
|
Seong, Jae-Dong |
|
2016 |
|
8 |
p. 1438-1447 |
artikel |
68 |
Multi-objective trade-off analysis of an integrated cold gas propulsion system
|
Banazadeh, Afshin |
|
2013 |
|
8 |
p. 1233-1250 |
artikel |
69 |
Multi-objective trajectory planning over terrain using label-setting greedy-based algorithm
|
Zardashti, R |
|
2015 |
|
8 |
p. 1435-1453 |
artikel |
70 |
Multiple failure prognosis of landing gear retraction/extension system based on H∞ filtering
|
Chen, Jie |
|
2015 |
|
8 |
p. 1543-1555 |
artikel |
71 |
New control methodology for a morphing wing demonstrator
|
Tchatchueng Kammegne, Michel Joël |
|
2018 |
|
8 |
p. 1479-1494 |
artikel |
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 |
artikel |
73 |
Nonlinear adaptive sliding mode tracking control of an airplane with wing damage
|
Asadi, D |
|
2018 |
|
8 |
p. 1405-1420 |
artikel |
74 |
Nonlinear dynamic modeling in low frequency and control system stability domain determination for a LPE
|
Jafargholi, Ali |
|
2016 |
|
8 |
p. 1467-1485 |
artikel |
75 |
Novel acquisition of global positioning system signals based on parameter prediction and the chirp z-transform
|
Xu, Bing |
|
2017 |
|
8 |
p. 1391-1401 |
artikel |
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 |
artikel |
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 |
artikel |
78 |
Numerical investigation of the axial compressor performance with inlet distortions
|
Liu, ZX |
|
2018 |
|
8 |
p. 1434-1441 |
artikel |
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 |
artikel |
80 |
Numerical modelling of a low Reynolds number plunging airfoil flow field characteristics
|
Amiralaei, Mohammad Reza |
|
2013 |
|
8 |
p. 1251-1264 |
artikel |
81 |
Numerical simulation of the airflow over a military aircraft with active intake
|
Triantafyllou, T |
|
2017 |
|
8 |
p. 1369-1390 |
artikel |
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 |
artikel |
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 |
artikel |
84 |
Numerical study on impulse characteristics of laser-supported air-breathing pulsed detonation thrusters
|
Li, Xiaokang |
|
2014 |
|
8 |
p. 1324-1335 |
artikel |
85 |
Oil damping energy loss analysis of landing gear shock absorber
|
Jiao, Fujun |
|
2019 |
|
8 |
p. 3096-3106 |
artikel |
86 |
Optimal impact angle control guidance law considering the seeker’s field-of-view limits
|
Park, Bong-Gyun |
|
2013 |
|
8 |
p. 1347-1364 |
artikel |
87 |
Optimal layout method of distributed locking device of satellite based on plant root growth theory
|
Wang, Gang |
|
2019 |
|
8 |
p. 2802-2818 |
artikel |
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 |
artikel |
89 |
Optimization of the aerodynamic drag reduction of a passenger hatchback car
|
Guo, Ziyu |
|
2019 |
|
8 |
p. 2819-2836 |
artikel |
90 |
Orbit design and control method for satellite clusters and its applications to NetSat project
|
Zhou, Liang |
|
2018 |
|
8 |
p. 1559-1570 |
artikel |
91 |
Parametric reduced-order model approach for simulation and optimization of aeroelastic systems with structural nonlinearities
|
Castellani, Michele |
|
2016 |
|
8 |
p. 1359-1370 |
artikel |
92 |
Performance investigation of a supersonic air intake in the presence of the boundary layer suction
|
Soltani, MR |
|
2015 |
|
8 |
p. 1495-1509 |
artikel |
93 |
Pigeon-inspired optimization and lateral inhibition for image matching of autonomous aerial refueling
|
Sun, Yongbin |
|
2018 |
|
8 |
p. 1571-1583 |
artikel |
94 |
Pose measurement of nozzle based on laser range finders for capturing satellite
|
Zhang, Yu |
|
2016 |
|
8 |
p. 1385-1396 |
artikel |
95 |
Position control of linear electromechanical actuator for spoiler system base on the inverse system method
|
Cui, Yebing |
|
2014 |
|
8 |
p. 1273-1282 |
artikel |
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 |
artikel |
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 |
artikel |
98 |
Radar track segmentation with cubic splines for collision risk models in high density terminal areas
|
Cózar, JA |
|
2015 |
|
8 |
p. 1371-1383 |
artikel |
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 |
artikel |
100 |
Receding horizon control of a 3 DOF helicopter using online estimation of aerodynamic parameters
|
Mehndiratta, Mohit |
|
2018 |
|
8 |
p. 1442-1453 |
artikel |
101 |
Regeneratively cooled scramjet heat transfer calculation and comparison with experimental data
|
Jiang, Jin |
|
2014 |
|
8 |
p. 1227-1234 |
artikel |
102 |
Research of the suction flow control on wings at low Reynolds numbers
|
Ma, Dongli |
|
2018 |
|
8 |
p. 1515-1528 |
artikel |
103 |
Research on generalized inertial navigation system damping technology based on dual-model mean
|
Hongyang, He |
|
2016 |
|
8 |
p. 1518-1527 |
artikel |
104 |
Robust finite-time line-of-sight angular rate estimation in missile guidance
|
He, Shaoming |
|
2017 |
|
8 |
p. 1550-1559 |
artikel |
105 |
Side force over slender body with rings at different location at subsonic speed
|
Kumar, P |
|
2017 |
|
8 |
p. 1478-1491 |
artikel |
106 |
Simple model-free attitude control design for flexible spacecraft with prescribed performance
|
Zhang, Chao |
|
2019 |
|
8 |
p. 2760-2771 |
artikel |
107 |
Spacecraft attitude dynamics simulator actuated by cold gas propulsion system
|
Mirshams, Mehran |
|
2015 |
|
8 |
p. 1510-1530 |
artikel |
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 |
artikel |
109 |
Statistical modelling for prediction of axis-switching in rectangular jets
|
Tipnis, Tanmay J |
|
2013 |
|
8 |
p. 1325-1337 |
artikel |
110 |
Supersonic viscous corner flows
|
Naidoo, P |
|
2012 |
|
8 |
p. 950-965 |
artikel |
111 |
The aerodynamic performance of a 2D lumped flexible airfoil in forward flight
|
Zhou, Chaoying |
|
2014 |
|
8 |
p. 1363-1374 |
artikel |
112 |
The design and performance evaluation of axial ventilator with honeycomb in the turbofan engine lubrication system
|
Jingyu, Zhao |
|
2016 |
|
8 |
p. 1397-1408 |
artikel |
113 |
The effect of different clearance geometry configurations on aerodynamic performance in a high-load compressor cascade
|
Chen, Shaowen |
|
2014 |
|
8 |
p. 1425-1433 |
artikel |
114 |
The GENUS aircraft conceptual design environment
|
Smith, H |
|
2019 |
|
8 |
p. 2932-2947 |
artikel |
115 |
The impact of circumferential casing grooves on rotating instability in a transonic axial compressor
|
Ye, Shubo |
|
2019 |
|
8 |
p. 2868-2893 |
artikel |
116 |
Theoretical investigation of the performance of alternative aviation fuels in an aero-engine combustion chamber
|
Uryga-Bugajska, I |
|
2011 |
|
8 |
p. 874-885 |
artikel |
117 |
Three-dimensional design and numerical simulation of magnetohydrodynamic controlled hypersonic inlets
|
Lu, H |
|
2012 |
|
8 |
p. 1002-1013 |
artikel |
118 |
Time accurate modelling of the secondary air system response to rapid transients
|
Gallar, L |
|
2011 |
|
8 |
p. 946-958 |
artikel |
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 |
artikel |
120 |
Tracking of spiraling reentry vehicles with varying frequency using a new target dynamic model
|
Ohlmeyer, Ernest J |
|
2014 |
|
8 |
p. 1235-1245 |
artikel |
121 |
Transitional flight equilibrium and performance study for the X-NMRL tail-sitter VTOL MAV
|
Tang, Wei |
|
2019 |
|
8 |
p. 3056-3077 |
artikel |
122 |
Two novel robust tracking control strategies for eliminating aircraft wing rock
|
Yin, Hang |
|
2019 |
|
8 |
p. 3042-3055 |
artikel |
123 |
Type-2 fuzzy adaptive sliding mode control of hypersonic flight
|
Jiao, Xin |
|
2019 |
|
8 |
p. 2731-2744 |
artikel |
124 |
Validation of an actuator disk model for numerical simulation of propeller
|
Li, Bo |
|
2015 |
|
8 |
p. 1454-1463 |
artikel |
125 |
Vibration and damping analysis of aerospace pipeline conveying fluid with constrained layer damping treatment
|
Gao, Pei-xin |
|
2018 |
|
8 |
p. 1529-1541 |
artikel |
126 |
Vision-based guidance for fixed-wing unmanned aerial vehicle autonomous carrier landing
|
Zhang, Zhouyu |
|
2019 |
|
8 |
p. 2894-2913 |
artikel |
127 |
Vision-based terrain referenced navigation of aerial vehicles using an adaptive extended Kalman filter
|
Mok, Sung-Hoon |
|
2018 |
|
8 |
p. 1584-1597 |
artikel |