| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active vibration suppression in flexible spacecraft with optical measurement
|
Wang, Zhaohui
|
|
2016
|
55 |
C |
p. 49-56
8 p.
|
artikel
|
| 2 |
Adaptive backstepping controller and sliding mode controller design for formation flight in Sun–Earth L 2 point
|
Wang, Feng
|
|
2016
|
55 |
C |
p. 409-418
10 p.
|
artikel
|
| 3 |
Adaptive interacting particle system algorithm for aircraft conflict probability estimation
|
Jacquemart, Damien
|
|
2016
|
55 |
C |
p. 431-438
8 p.
|
artikel
|
| 4 |
A dynamic air traffic model for analyzing relationship patterns of traffic flow parameters in terminal airspace
|
Xu, Yan
|
|
2016
|
55 |
C |
p. 10-23
14 p.
|
artikel
|
| 5 |
Aerodynamic shape optimization for minimum robust drag and lift reliability constraint
|
Papadimitriou, Dimitrios I.
|
|
2016
|
55 |
C |
p. 24-33
10 p.
|
artikel
|
| 6 |
A hybrid evaluation model for flight performance based on bacterial foraging and Elman network
|
Wu, Qi
|
|
2016
|
55 |
C |
p. 392-399
8 p.
|
artikel
|
| 7 |
Airplane loss of control problem: Linear controllability analysis
|
Hassan, Ahmed M.
|
|
2016
|
55 |
C |
p. 264-271
8 p.
|
artikel
|
| 8 |
Analytical solution for thermal buckling analysis of rectangular plates with functionally graded coatings
|
Thang, Pham Toan
|
|
2016
|
55 |
C |
p. 465-473
9 p.
|
artikel
|
| 9 |
Application of efficient surrogate modeling to aeroelastic analyses of an aircraft wing
|
Sommerwerk, K.
|
|
2016
|
55 |
C |
p. 314-323
10 p.
|
artikel
|
| 10 |
A study on nonlinear vibration behavior of CNT-based representative volume element
|
Jamal-Omidi, Majid
|
|
2016
|
55 |
C |
p. 272-281
10 p.
|
artikel
|
| 11 |
Automatic modelling of airfoil data points
|
Pérez-Arribas, F.
|
|
2016
|
55 |
C |
p. 449-457
9 p.
|
artikel
|
| 12 |
Computational framework for Launch, Ascent, and Vehicle Aerodynamics (LAVA)
|
Kiris, Cetin C.
|
|
2016
|
55 |
C |
p. 189-219
31 p.
|
artikel
|
| 13 |
Conceptual Remote Sensing Satellite Design Optimization under uncertainty
|
Jafarsalehi, A.
|
|
2016
|
55 |
C |
p. 377-391
15 p.
|
artikel
|
| 14 |
Constrained dual-loop attitude control design for spacecraft
|
Li, Mingxiang
|
|
2016
|
55 |
C |
p. 170-176
7 p.
|
artikel
|
| 15 |
Correlation of mission type to cyclic loading as a basis for agile military aircraft asset management
|
Newcamp, Jeffrey
|
|
2016
|
55 |
C |
p. 111-119
9 p.
|
artikel
|
| 16 |
Direct image-based visual servoing of free-floating space manipulators
|
Alepuz, Javier Pérez
|
|
2016
|
55 |
C |
p. 1-9
9 p.
|
artikel
|
| 17 |
Dynamic modeling and vibration control of a flexible aerial refueling hose
|
Liu, Zhijie
|
|
2016
|
55 |
C |
p. 92-102
11 p.
|
artikel
|
| 18 |
Earth–Moon transfer with near-optimal lunar capture in the restricted four-body problem
|
Qi, Yi
|
|
2016
|
55 |
C |
p. 282-291
10 p.
|
artikel
|
| 19 |
Editorial Board
|
|
|
2016
|
55 |
C |
p. IFC-
1 p.
|
artikel
|
| 20 |
Experimental study on the effects of wing sweep on Gurney flap performance
|
Traub, Lance W.
|
|
2016
|
55 |
C |
p. 57-63
7 p.
|
artikel
|
| 21 |
Finite element implementation of Puck's failure criterion for failure analysis of laminated plate subjected to biaxial loadings
|
Gadade, Appaso M.
|
|
2016
|
55 |
C |
p. 227-241
15 p.
|
artikel
|
| 22 |
Fuel weight estimates of military turbo-propeller transport aircraft
|
Marinus, Benoît G.
|
|
2016
|
55 |
C |
p. 458-464
7 p.
|
artikel
|
| 23 |
Full-altitude attitude angles envelope and model predictive control-based attitude angles protection for civil aircraft
|
Dong, Yiqun
|
|
2016
|
55 |
C |
p. 292-306
15 p.
|
artikel
|
| 24 |
Fuselage aerodynamic prediction methods
|
Nicolosi, Fabrizio
|
|
2016
|
55 |
C |
p. 332-343
12 p.
|
artikel
|
| 25 |
Ground experimentation with 3D printed scramjet inlet models at hypervelocities
|
Rêgo, I.S.
|
|
2016
|
55 |
C |
p. 307-313
7 p.
|
artikel
|
| 26 |
Gyro-free attitude and rate estimation for a small satellite using SVD and EKF
|
Hajiyev, Chingiz
|
|
2016
|
55 |
C |
p. 324-331
8 p.
|
artikel
|
| 27 |
Helicopter blade reliability: Statistical data analysis and modeling
|
Shahani, A.R.
|
|
2016
|
55 |
C |
p. 43-48
6 p.
|
artikel
|
| 28 |
Influence of main and outer wings on aerodynamic characteristics of compound wing-in-ground effect
|
Tavakoli Dakhrabadi, M.
|
|
2016
|
55 |
C |
p. 177-188
12 p.
|
artikel
|
| 29 |
Influence of water ingress onto the crack propagation rate in a AA2024-T3 plate repaired by a carbon/epoxy patch
|
Rezgani, L.
|
|
2016
|
55 |
C |
p. 359-365
7 p.
|
artikel
|
| 30 |
Inverse design of shock wave distortion for a direct-connect facility
|
Yu, Kaikai
|
|
2016
|
55 |
C |
p. 220-226
7 p.
|
artikel
|
| 31 |
LIDAR obstacle warning and avoidance system for unmanned aerial vehicle sense-and-avoid
|
Ramasamy, Subramanian
|
|
2016
|
55 |
C |
p. 344-358
15 p.
|
artikel
|
| 32 |
Mechanical properties and fracture analysis of functionalized carbon nanotube embedded by polymer matrix
|
Esbati, Amir Hossein
|
|
2016
|
55 |
C |
p. 120-130
11 p.
|
artikel
|
| 33 |
Minimum-time trajectories of electric sail with advanced thrust model
|
Quarta, Alessandro A.
|
|
2016
|
55 |
C |
p. 419-430
12 p.
|
artikel
|
| 34 |
Morphing elastically lofted transition for active camber control surfaces
|
Woods, Benjamin K.S.
|
|
2016
|
55 |
C |
p. 439-448
10 p.
|
artikel
|
| 35 |
Multi-UAVs tracking target in urban environment by model predictive control and Improved Grey Wolf Optimizer
|
Yao, Peng
|
|
2016
|
55 |
C |
p. 131-143
13 p.
|
artikel
|
| 36 |
Nonlinear buckling analysis of the conical and cylindrical shells using the SGL strain based reduced order model and the PHC method
|
Liang, Ke
|
|
2016
|
55 |
C |
p. 103-110
8 p.
|
artikel
|
| 37 |
Numerical investigation of the effect of stagger on the aerodynamic characteristics of a Busemann biplane
|
Patidar, Vijay Kumar
|
|
2016
|
55 |
C |
p. 252-263
12 p.
|
artikel
|
| 38 |
Numerical simulation of pararotor dynamics: Effect of mass displacement from blade plane
|
Piechocki, Joaquín
|
|
2016
|
55 |
C |
p. 400-408
9 p.
|
artikel
|
| 39 |
Optimal design of wind turbine airfoils based on functional integral and curvature smooth continuous theory
|
Wang, Quan
|
|
2016
|
55 |
C |
p. 34-42
9 p.
|
artikel
|
| 40 |
Pseudo-analytic approach to determine optimal conditions for maximizing altitude of sounding rocket
|
Lee, Sang-Hyeon
|
|
2016
|
55 |
C |
p. 64-75
12 p.
|
artikel
|
| 41 |
Reduction of end wall loss in axial compressor by using non-axisymmetric profiled end wall: A new design approach based on end wall velocity modification
|
Chu, Wuli
|
|
2016
|
55 |
C |
p. 76-91
16 p.
|
artikel
|
| 42 |
Robust H ∞ filtering for a spacecraft attitude determination system with affine LPV approach
|
Yang, Shujie
|
|
2016
|
55 |
C |
p. 158-169
12 p.
|
artikel
|
| 43 |
Semi-analytical approach for computing near-optimal low-thrust transfers to geosynchronous orbit
|
Zhang, Lei
|
|
2016
|
55 |
C |
p. 482-493
12 p.
|
artikel
|
| 44 |
Smooth finite-time fault-tolerant attitude tracking control for rigid spacecraft
|
Hu, Qinglei
|
|
2016
|
55 |
C |
p. 144-157
14 p.
|
artikel
|
| 45 |
Symmetrical and non-symmetrical 3D wing deformation of flapping micro aerial vehicles
|
Tay, W.B.
|
|
2016
|
55 |
C |
p. 242-251
10 p.
|
artikel
|
| 46 |
Terminal height estimation using a Fading Gaussian Deterministic filter
|
de Angelis, Emanuele L.
|
|
2016
|
55 |
C |
p. 366-376
11 p.
|
artikel
|
| 47 |
The modified Brazier approach to predict the collapse load of a stiffened circular composite spar under bending load
|
Kim, Sung Joon
|
|
2016
|
55 |
C |
p. 474-481
8 p.
|
artikel
|
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