| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active cancellation analysis based on the radar detection probability
|
Yi, Mingxu
|
|
2015
|
46 |
C |
p. 273-281
9 p.
|
artikel
|
| 2 |
Adaptation and optimization of the synchronization gains in the adaptive spacecraft attitude synchronization
|
Zhang, Kewen
|
|
2015
|
46 |
C |
p. 116-123
8 p.
|
artikel
|
| 3 |
Adaptive sliding mode control for spacecraft body-fixed hovering in the proximity of an asteroid
|
Lee, Daero
|
|
2015
|
46 |
C |
p. 471-483
13 p.
|
artikel
|
| 4 |
Adaptive square-root cubature–quadrature Kalman particle filter via KLD-sampling for orbit determination
|
Kiani, M.
|
|
2015
|
46 |
C |
p. 159-167
9 p.
|
artikel
|
| 5 |
Adjoint-based adaptive finite element method for the compressible Euler equations using finite calculus
|
Kouhi, Mohammad
|
|
2015
|
46 |
C |
p. 422-435
14 p.
|
artikel
|
| 6 |
Aerodynamic performance of transonic axial compressor with a casing groove combined with blade tip injection and ejection
|
Dinh, Cong-Truong
|
|
2015
|
46 |
C |
p. 176-187
12 p.
|
artikel
|
| 7 |
A fuzzy-based gas turbine fault detection and identification system for full and part-load performance deterioration
|
Mohammadi, Ehsan
|
|
2015
|
46 |
C |
p. 82-93
12 p.
|
artikel
|
| 8 |
Analytic approach to determine optimal conditions for maximizing altitude of sounding rocket: Flight in standard atmosphere
|
Lee, Sang-Hyeon
|
|
2015
|
46 |
C |
p. 374-385
12 p.
|
artikel
|
| 9 |
An assessment of distributed propulsion: Advanced propulsion system architectures for conventional aircraft configurations
|
Kirner, Rudi
|
|
2015
|
46 |
C |
p. 42-50
9 p.
|
artikel
|
| 10 |
Application of H2/H∞ and dynamic inversion techniques to aircraft landing control
|
Lungu, Romulus
|
|
2015
|
46 |
C |
p. 146-158
13 p.
|
artikel
|
| 11 |
Application of multi-stage multi-objective multi-disciplinary agent model based on dynamic substructural method in Mistuned Blisk
|
Bai, Bin
|
|
2015
|
46 |
C |
p. 104-115
12 p.
|
artikel
|
| 12 |
A sparse representation-based optimization algorithm for measuring the time delay of pulsar integrated pulse profile
|
Yu, Hang
|
|
2015
|
46 |
C |
p. 94-103
10 p.
|
artikel
|
| 13 |
Attitude stabilization of rigid spacecraft with minimal attitude coordinates and unknown time-varying delay
|
Samiei, Ehsan
|
|
2015
|
46 |
C |
p. 412-421
10 p.
|
artikel
|
| 14 |
Boost-skipping trajectory optimization for air-breathing hypersonic missile
|
Chai, Dong
|
|
2015
|
46 |
C |
p. 506-513
8 p.
|
artikel
|
| 15 |
Bounds on maximal and minimal distances for coplanar satellite relative motion under given initial conditions
|
Dang, Zhaohui
|
|
2015
|
46 |
C |
p. 204-209
6 p.
|
artikel
|
| 16 |
Combustion characteristics of hybrid rocket motor with segmented grain
|
Tian, Hui
|
|
2015
|
46 |
C |
p. 537-547
11 p.
|
artikel
|
| 17 |
Contribution of simulated space VLBI to the Chang'E-1 orbit determination and EOPs estimation
|
Wei, Erhu
|
|
2015
|
46 |
C |
p. 256-263
8 p.
|
artikel
|
| 18 |
Design of adaptive transonic laminar airfoils using the γ - Re ˜ θ t transition model
|
Robitaille, Martin
|
|
2015
|
46 |
C |
p. 60-71
12 p.
|
artikel
|
| 19 |
Design of three-dimensional nonlinear guidance law with bounded acceleration command
|
Du, Runle
|
|
2015
|
46 |
C |
p. 168-175
8 p.
|
artikel
|
| 20 |
Detailed investigation of flow and thermal field in micro/nano nozzles using Simplified Bernoulli Trial (SBT) collision scheme in DSMC
|
Saadati, Seyed Ali
|
|
2015
|
46 |
C |
p. 236-255
20 p.
|
artikel
|
| 21 |
Diagnostic and decision support systems by identification of abnormal events: Application to helicopters
|
Bect, Pierre
|
|
2015
|
46 |
C |
p. 339-350
12 p.
|
artikel
|
| 22 |
Distributed cooperative guidance of multiple anti-ship missiles with arbitrary impact angle constraint
|
Wang, Xingliang
|
|
2015
|
46 |
C |
p. 299-311
13 p.
|
artikel
|
| 23 |
Dynamic response of aerospace structures by means of refined beam theories
|
Pagani, A.
|
|
2015
|
46 |
C |
p. 360-373
14 p.
|
artikel
|
| 24 |
Editorial Board
|
|
|
2015
|
46 |
C |
p. IFC-
1 p.
|
artikel
|
| 25 |
Enhanced trajectory linearization control based advanced guidance and control for hypersonic reentry vehicle with multiple disturbances
|
Shao, Xingling
|
|
2015
|
46 |
C |
p. 523-536
14 p.
|
artikel
|
| 26 |
Experimental and computational study on combustion performance of a kerosene fueled dual-mode scramjet engine
|
Tian, Ye
|
|
2015
|
46 |
C |
p. 451-458
8 p.
|
artikel
|
| 27 |
Experimental and numerical investigations of combustion mode transition in a direct–connect scramjet combustor
|
Xiao, Baoguo
|
|
2015
|
46 |
C |
p. 331-338
8 p.
|
artikel
|
| 28 |
FDOA post-Newtonian equations for the location of passive emitters placed in the vicinity of the Earth
|
Gambi, J.M.
|
|
2015
|
46 |
C |
p. 137-145
9 p.
|
artikel
|
| 29 |
Flexure of power law governed functionally graded plates using ABAQUS UMAT
|
Shiyekar, S.M.
|
|
2015
|
46 |
C |
p. 51-59
9 p.
|
artikel
|
| 30 |
Guaranteed cost robust weighted measurement fusion steady-state Kalman predictors with uncertain noise variances
|
Yang, Chunshan
|
|
2015
|
46 |
C |
p. 459-470
12 p.
|
artikel
|
| 31 |
Immunity-based flight envelope prediction at post-failure conditions
|
Perhinschi, Mario George
|
|
2015
|
46 |
C |
p. 264-272
9 p.
|
artikel
|
| 32 |
Influence of tapered tether on cislunar payload transmission system and energy analysis
|
Yang, Yong
|
|
2015
|
46 |
C |
p. 210-220
11 p.
|
artikel
|
| 33 |
In search of technology readiness level (TRL) 10
|
Straub, Jeremy
|
|
2015
|
46 |
C |
p. 312-320
9 p.
|
artikel
|
| 34 |
Inverse design of inlet distortion using method of characteristics for direct-connect scramjet studies
|
Yu, Kaikai
|
|
2015
|
46 |
C |
p. 351-359
9 p.
|
artikel
|
| 35 |
Lanthanum doping for longevity of alumina catalyst bed in hydrogen peroxide thruster
|
Kang, Shinjae
|
|
2015
|
46 |
C |
p. 197-203
7 p.
|
artikel
|
| 36 |
Long dwell time orbits for lander-based Mars missions
|
Ortore, Emiliano
|
|
2015
|
46 |
C |
p. 1-11
11 p.
|
artikel
|
| 37 |
Multiple stage satellite launch vehicle ascent optimization using Chebyshev wavelets
|
Shahmirzaee Jeshvaghani, Sedigheh
|
|
2015
|
46 |
C |
p. 321-330
10 p.
|
artikel
|
| 38 |
Numerical study of non-equilibrium condensation and shock waves in transonic moist-air and steam flows
|
Hamidi, S.
|
|
2015
|
46 |
C |
p. 188-196
9 p.
|
artikel
|
| 39 |
On application of high-order compact finite-difference schemes to compressible vorticity confinement method
|
Sadri, Maryam
|
|
2015
|
46 |
C |
p. 398-411
14 p.
|
artikel
|
| 40 |
On heat and mass transfer analysis for the flow of a nanofluid between rotating parallel plates
|
Mohyud-Din, Syed Tauseef
|
|
2015
|
46 |
C |
p. 514-522
9 p.
|
artikel
|
| 41 |
Optimal orbits around Ganymede for the JUICE mission
|
Ortore, Emiliano
|
|
2015
|
46 |
C |
p. 282-286
5 p.
|
artikel
|
| 42 |
Parallel packing code for propellant microstructure analysis
|
Baietta, Alessandro
|
|
2015
|
46 |
C |
p. 484-492
9 p.
|
artikel
|
| 43 |
Potential field based receding horizon motion planning for centrality-aware multiple UAV cooperative surveillance
|
Di, Bin
|
|
2015
|
46 |
C |
p. 386-397
12 p.
|
artikel
|
| 44 |
Prediction of stability behaviors of longitudinal and circumferential eigenmodes in a choked thermoacoustic combustor
|
Li, Lei
|
|
2015
|
46 |
C |
p. 12-21
10 p.
|
artikel
|
| 45 |
Radar/electro-optical data fusion for non-cooperative UAS sense and avoid
|
Fasano, Giancarmine
|
|
2015
|
46 |
C |
p. 436-450
15 p.
|
artikel
|
| 46 |
Random weighting method for estimation of error characteristics in SINS/GPS/SAR integrated navigation system
|
Gao, Shesheng
|
|
2015
|
46 |
C |
p. 22-29
8 p.
|
artikel
|
| 47 |
Stability characteristics of the single-engine tractor propeller airplane in climb
|
Milenković-Babić, Miodrag
|
|
2015
|
46 |
C |
p. 227-235
9 p.
|
artikel
|
| 48 |
Statistical gain-scheduling method for aircraft flight simulation
|
Choi, Youngjun
|
|
2015
|
46 |
C |
p. 493-505
13 p.
|
artikel
|
| 49 |
Study on longitudinal stability improvement of flying wing aircraft based on synthetic jet flow control
|
Xu, Xiaoping
|
|
2015
|
46 |
C |
p. 287-298
12 p.
|
artikel
|
| 50 |
Systematic design of tape spring hinges for solar array by optimization method considering deployment performances
|
Kim, Kyung-Won
|
|
2015
|
46 |
C |
p. 124-136
13 p.
|
artikel
|
| 51 |
The impact of control allocation on trim drag of blended wing body aircraft
|
Huijts, Crispijn
|
|
2015
|
46 |
C |
p. 72-81
10 p.
|
artikel
|
| 52 |
The postbuckling behaviour of adhesively bonded stiffened panels subjected to in-plane shear loading
|
de Paula Guedes Villani, Anaisa
|
|
2015
|
46 |
C |
p. 30-41
12 p.
|
artikel
|
| 53 |
Two stage switching control for autonomous formation flight of unmanned aerial vehicles
|
Ambroziak, Leszek
|
|
2015
|
46 |
C |
p. 221-226
6 p.
|
artikel
|
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