| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Acceleration autopilot design for gliding guided projectiles with less measurement information
|
Xu, Qiuping
|
|
2018
|
77 |
C |
p. 256-264
|
artikel
|
| 2 |
Acceleration autopilot for a guided spinning rocket via adaptive output feedback
|
Zhao, Liangyu
|
|
2018
|
77 |
C |
p. 573-584
|
artikel
|
| 3 |
Aerodynamic optimization of helicopter rear fuselage
|
Batrakov, A.S.
|
|
2018
|
77 |
C |
p. 704-712
|
artikel
|
| 4 |
A flexible multi-disciplinary environment for performance, life-cycle cost, and safety evaluation of suborbital vehicles
|
Frank, Christopher P.
|
|
2018
|
77 |
C |
p. 555-562
|
artikel
|
| 5 |
A MIMO data driven control to suppress structural vibrations
|
Xie, Yangmin
|
|
2018
|
77 |
C |
p. 429-438
|
artikel
|
| 6 |
An active disturbance rejection control guidance law based collision avoidance for unmanned aerial vehicles
|
Zhang, Ning
|
|
2018
|
77 |
C |
p. 658-669
|
artikel
|
| 7 |
Analysis of pressure fluctuation in transonic cavity flows using modal decomposition
|
Liu, Hongkang
|
|
2018
|
77 |
C |
p. 819-835
|
artikel
|
| 8 |
An application of Deep Neural Networks to the in-flight parameter identification for detection and characterization of aircraft icing
|
Dong, Yiqun
|
|
2018
|
77 |
C |
p. 34-49
|
artikel
|
| 9 |
A new direct filtering approach to INS/GNSS integration
|
Hu, Gaoge
|
|
2018
|
77 |
C |
p. 755-764
|
artikel
|
| 10 |
An extended unsteady aerodynamic model at high angles of attack
|
Mi, Bai-gang
|
|
2018
|
77 |
C |
p. 788-801
|
artikel
|
| 11 |
An integrated load sensing valve-controlled actuator based on power-by-wire for aircraft structural test
|
Shang, Yaoxing
|
|
2018
|
77 |
C |
p. 117-128
|
artikel
|
| 12 |
An offset hub active vibration control system for mitigating helicopter vibrations during power loss: Simulation and experimental demonstration
|
Kakaley, Daniel E.
|
|
2018
|
77 |
C |
p. 610-625
|
artikel
|
| 13 |
A novel TE-material based thermal protection structure and its performance evaluation for hypersonic flight vehicles
|
Gong, Chun-Lin
|
|
2018
|
77 |
C |
p. 458-470
|
artikel
|
| 14 |
Axisymmetric nonlinear vibration analysis of sandwich annular plates with FG-CNTRC face sheets based on the higher-order shear deformation plate theory
|
Ansari, R.
|
|
2018
|
77 |
C |
p. 306-319
|
artikel
|
| 15 |
Characteristics of nonlinear vibration of nanocomposite cylindrical shells with piezoelectric actuators under thermo-mechanical loads
|
Ninh, Dinh Gia
|
|
2018
|
77 |
C |
p. 595-609
|
artikel
|
| 16 |
Combustion stabilizations in a liquid kerosene fueled supersonic combustor equipped with an integrated pilot strut
|
Zhang, Junlong
|
|
2018
|
77 |
C |
p. 83-91
|
artikel
|
| 17 |
Correction of low-Reynolds number turbulence model to hydrocarbon fuel at supercritical pressure
|
Tao, Zhi
|
|
2018
|
77 |
C |
p. 156-167
|
artikel
|
| 18 |
Covariance analysis of Lambert's problem via Lagrange's transfer-time formulation
|
Zhang, Gang
|
|
2018
|
77 |
C |
p. 765-773
|
artikel
|
| 19 |
Data-driven risk assessment and multicriteria optimization of UAV operations
|
Rubio-Hervas, Jaime
|
|
2018
|
77 |
C |
p. 510-523
|
artikel
|
| 20 |
Dealiasing harmonic balance method for obtaining periodic solutions of an aeroelastic system
|
Dai, Honghua
|
|
2018
|
77 |
C |
p. 244-255
|
artikel
|
| 21 |
Design of a variable Mach number wind tunnel nozzle operated by a single jack
|
Lv, Zheng
|
|
2018
|
77 |
C |
p. 299-305
|
artikel
|
| 22 |
Development of an optimized trend kriging model using regression analysis and selection process for optimal subset of basis functions
|
Lee, Hakjin
|
|
2018
|
77 |
C |
p. 273-285
|
artikel
|
| 23 |
Disturbance observer based reliable H ∞ fuzzy attitude tracking control for Mars entry vehicles with actuator failures
|
Wu, Huai-Ning
|
|
2018
|
77 |
C |
p. 92-104
|
artikel
|
| 24 |
Drag and heat reduction efficiency research on opposing jet in supersonic flows
|
Shen, BinXian
|
|
2018
|
77 |
C |
p. 696-703
|
artikel
|
| 25 |
Dynamic analysis of assembled aircraft structures considering interfaces with nonlinear behavior
|
Hernández, Santiago
|
|
2018
|
77 |
C |
p. 265-272
|
artikel
|
| 26 |
Dynamic snap-through of shallow arches under thermal shock
|
Keibolahi, A.
|
|
2018
|
77 |
C |
p. 545-554
|
artikel
|
| 27 |
Editorial Board
|
|
|
2018
|
77 |
C |
p. ii
|
artikel
|
| 28 |
Effect of extended necks on transmission loss performances of Helmholtz resonators in presence of a grazing flow
|
Zhao, He
|
|
2018
|
77 |
C |
p. 228-234
|
artikel
|
| 29 |
Equations of motion for optimal maneuvering with global aerodynamic model
|
Morales, Mauricio A.V.
|
|
2018
|
77 |
C |
p. 206-216
|
artikel
|
| 30 |
Experimental and numerical investigation of combustion characteristics on GO2/GH2 shear coaxial injector
|
Dai, Jian
|
|
2018
|
77 |
C |
p. 725-732
|
artikel
|
| 31 |
Extending slide-slip mesh update method to finite volume method
|
Qu, Kun
|
|
2018
|
77 |
C |
p. 50-57
|
artikel
|
| 32 |
Failure effect analysis and reconfiguration of thrusters based on inverse simulation of manually controlled RVD
|
Zhou, Wanmeng
|
|
2018
|
77 |
C |
p. 485-498
|
artikel
|
| 33 |
Forced motions design for aerodynamic identification and modeling of a generic missile configuration
|
Allen, Jacob
|
|
2018
|
77 |
C |
p. 742-754
|
artikel
|
| 34 |
Generation and control of monodisperse bubble suspensions in microgravity
|
Bitlloch, Pau
|
|
2018
|
77 |
C |
p. 344-352
|
artikel
|
| 35 |
Grey wolf optimization based sense and avoid algorithm in a Bayesian framework for multiple UAV path planning in an uncertain environment
|
Radmanesh, Mohammadreza
|
|
2018
|
77 |
C |
p. 168-179
|
artikel
|
| 36 |
Hybridized attitude determination techniques to improve ballistic projectile navigation, guidance and control
|
de Celis, Raúl
|
|
2018
|
77 |
C |
p. 138-148
|
artikel
|
| 37 |
Hybrid reliability analysis and optimization for spacecraft structural system with random and fuzzy parameters
|
Wang, Chong
|
|
2018
|
77 |
C |
p. 353-361
|
artikel
|
| 38 |
Identification of the formation of resonant tones in compressible cavity flows
|
Bacci, David
|
|
2018
|
77 |
C |
p. 320-331
|
artikel
|
| 39 |
Improved polar inertial navigation algorithm based on pseudo INS mechanization
|
Liu, Meng
|
|
2018
|
77 |
C |
p. 105-116
|
artikel
|
| 40 |
Influence of tip leakage flow and ejection on stall mechanism in a transonic tandem rotor
|
Han, Le
|
|
2018
|
77 |
C |
p. 499-509
|
artikel
|
| 41 |
Low-speed preconditioning for strongly coupled integration of Reynolds-averaged Navier–Stokes equations and two-equation turbulence models
|
Campobasso, M.S.
|
|
2018
|
77 |
C |
p. 286-298
|
artikel
|
| 42 |
Mode decoupling robust eigenstructure assignment applied to the lateral-directional dynamics of the F-16 aircraft
|
Albostan, Onur
|
|
2018
|
77 |
C |
p. 677-687
|
artikel
|
| 43 |
Multiobjective trajectory optimization for a suborbital spaceplane using Directed Search Domain approach
|
Wang, Kaiqiang
|
|
2018
|
77 |
C |
p. 713-724
|
artikel
|
| 44 |
Multirotor aircraft formation flight control with collision avoidance capability
|
de Angelis, Emanuele L.
|
|
2018
|
77 |
C |
p. 733-741
|
artikel
|
| 45 |
Nonlinear identification via connected neural networks for unsteady aerodynamic analysis
|
Winter, Maximilian
|
|
2018
|
77 |
C |
p. 802-818
|
artikel
|
| 46 |
Nonlinear thermomechanical buckling and post-buckling response of porous FGM plates using Reddy's HSDT
|
Cong, Pham Hong
|
|
2018
|
77 |
C |
p. 419-428
|
artikel
|
| 47 |
Nonorthogonality analysis of acoustics and vorticity modes: Should thermoacoustic energy norm be time-invariant?
|
Li, Lei
|
|
2018
|
77 |
C |
p. 149-155
|
artikel
|
| 48 |
Numerical study on solid-fuel scramjet combustor with fuel-rich hot gas
|
Zhao, Xiang
|
|
2018
|
77 |
C |
p. 25-33
|
artikel
|
| 49 |
Numerical study on the aerodynamic coupling effects of spinning and coning motions for a finned vehicle
|
Lu, Tianyu
|
|
2018
|
77 |
C |
p. 399-408
|
artikel
|
| 50 |
Online four dimensional trajectory prediction method based on aircraft intent updating
|
Zhang, Junfeng
|
|
2018
|
77 |
C |
p. 774-787
|
artikel
|
| 51 |
Optimal direct adaptive soft switching multi-model predictive control using the gap metric for spacecraft attitude control in a wide range of operating points
|
Saki, Saman
|
|
2018
|
77 |
C |
p. 235-243
|
artikel
|
| 52 |
Optimal formation reconfiguration of satellites under attitude constraints using only thrusters
|
Yoshimura, Yasuhiro
|
|
2018
|
77 |
C |
p. 449-457
|
artikel
|
| 53 |
Optimisation of adaptive shock control bumps with structural constraints
|
Jinks, Edward
|
|
2018
|
77 |
C |
p. 332-343
|
artikel
|
| 54 |
Performance assessment of a multi-fuel hybrid engine for future aircraft
|
Yin, Feijia
|
|
2018
|
77 |
C |
p. 217-227
|
artikel
|
| 55 |
Performance assessment of electrically driven pump-fed LOX/kerosene cycle rocket engine: Comparison with gas generator cycle
|
Kwak, Hyun-Duck
|
|
2018
|
77 |
C |
p. 67-82
|
artikel
|
| 56 |
Performance of radial–axial clearance rim seal in realistic working conditions
|
Jia, Xingyun
|
|
2018
|
77 |
C |
p. 373-387
|
artikel
|
| 57 |
Reachable set computation for spacecraft relative motion with energy-limited low-thrust
|
Lee, Sangjin
|
|
2018
|
77 |
C |
p. 180-188
|
artikel
|
| 58 |
Real-time collision avoidance maneuvers for spacecraft proximity operations via discrete-time Hamilton–Jacobi theory
|
Lee, Kwangwon
|
|
2018
|
77 |
C |
p. 688-695
|
artikel
|
| 59 |
Receding horizon guidance of a small unmanned aerial vehicle for planar reference path following
|
Hamada, Yoshiro
|
|
2018
|
77 |
C |
p. 129-137
|
artikel
|
| 60 |
Rectangular and skew shear buckling of FG-CNT reinforced composite skew plates using Ritz method
|
Kiani, Y.
|
|
2018
|
77 |
C |
p. 388-398
|
artikel
|
| 61 |
Reduction of transonic buffet onset for a wing with activated elasticity
|
Gao, Chuanqiang
|
|
2018
|
77 |
C |
p. 670-676
|
artikel
|
| 62 |
Refractive sail and its applications in solar sailing
|
Firuzi, Shahin
|
|
2018
|
77 |
C |
p. 362-372
|
artikel
|
| 63 |
Robust distributed consensus for deployment of Tethered Space Net Robot
|
Liu, Ya
|
|
2018
|
77 |
C |
p. 524-533
|
artikel
|
| 64 |
Robust finite-time guidance against maneuverable targets with unpredictable evasive strategies
|
Zhang, Ran
|
|
2018
|
77 |
C |
p. 534-544
|
artikel
|
| 65 |
Safe control of trailing UAV in close formation flight against actuator fault and wake vortex effect
|
Yu, Ziquan
|
|
2018
|
77 |
C |
p. 189-205
|
artikel
|
| 66 |
Simulation on flow control strategy of synthetic jet in an vertical axis wind turbine
|
Zhu, Haitian
|
|
2018
|
77 |
C |
p. 439-448
|
artikel
|
| 67 |
Spacecraft design optimisation for demise and survivability
|
Trisolini, Mirko
|
|
2018
|
77 |
C |
p. 638-657
|
artikel
|
| 68 |
Starting characteristics and phenomenon of a supersonic wind tunnel coupled with inlet model
|
Yu, Kaikai
|
|
2018
|
77 |
C |
p. 626-637
|
artikel
|
| 69 |
Statistical evaluation of performance impact of manufacturing variability by an adjoint method
|
Luo, Jiaqi
|
|
2018
|
77 |
C |
p. 471-484
|
artikel
|
| 70 |
Steepest descent quaternion attitude estimator
|
Zagorski, Pawel
|
|
2018
|
77 |
C |
p. 1-10
|
artikel
|
| 71 |
Studies on effusion cooling: Impact of geometric parameters on cooling effectiveness and coolant consumption
|
Venkatesh, Vishal
|
|
2018
|
77 |
C |
p. 58-66
|
artikel
|
| 72 |
Tube-based robust model predictive control for spacecraft proximity operations in the presence of persistent disturbance
|
Mammarella, M.
|
|
2018
|
77 |
C |
p. 585-594
|
artikel
|
| 73 |
Two-degree-of-freedom attitude tracking control for bank-to-turn aerial vehicles: An additive-state-decomposition-based method
|
Ren, Jinrui
|
|
2018
|
77 |
C |
p. 409-418
|
artikel
|
| 74 |
Uncertainty propagation in aerodynamic forces and heating analysis for hypersonic vehicles with uncertain-but-bounded geometric parameters
|
Zheng, Yuning
|
|
2018
|
77 |
C |
p. 11-24
|
artikel
|
| 75 |
Vibration control for a flexible satellite with input constraint based on Nussbaum function via backstepping method
|
Ji, Ning
|
|
2018
|
77 |
C |
p. 563-572
|
artikel
|
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