| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active robust control of uncertainty and flexibility suppression for air-breathing hypersonic vehicles
|
Pu, Zhiqiang
|
|
2015
|
42 |
C |
p. 429-441
13 p.
|
artikel
|
| 2 |
Adaptive velocity synchronization compound control of electro-hydraulic load simulator
|
Wang, Chengwen
|
|
2015
|
42 |
C |
p. 309-321
13 p.
|
artikel
|
| 3 |
Aerodynamic design optimization of helicopter rotor blades including airfoil shape for forward flight
|
Vu, N.A.
|
|
2015
|
42 |
C |
p. 106-117
12 p.
|
artikel
|
| 4 |
Aeroelastic analysis and active flutter suppression of an electro-rheological sandwich cylindrical panel under yawed supersonic flow
|
Hasheminejad, Seyyed M.
|
|
2015
|
42 |
C |
p. 118-127
10 p.
|
artikel
|
| 5 |
A high accuracy multiplex two-position alignment method based on SINS with the aid of star sensor
|
Wang, Xinlong
|
|
2015
|
42 |
C |
p. 66-73
8 p.
|
artikel
|
| 6 |
A parametric study of fixed-wing aircraft perching maneuvers
|
Venkateswara Rao, D.M.K.K.
|
|
2015
|
42 |
C |
p. 459-469
11 p.
|
artikel
|
| 7 |
Artificial neural network based inverse design: Airfoils and wings
|
Sun, Gang
|
|
2015
|
42 |
C |
p. 415-428
14 p.
|
artikel
|
| 8 |
Concurrent subspace design optimization and analysis of hypersonic vehicles based on response surface models
|
Zhang, Dong
|
|
2015
|
42 |
C |
p. 39-49
11 p.
|
artikel
|
| 9 |
Condition-based flight control for helicopters: An extension to condition-based maintenance
|
Voskuijl, Mark
|
|
2015
|
42 |
C |
p. 322-333
12 p.
|
artikel
|
| 10 |
Deployment and control of spacecraft solar array considering joint stick-slip friction
|
Li, Hai-Quan
|
|
2015
|
42 |
C |
p. 342-352
11 p.
|
artikel
|
| 11 |
Design and optimization of low-thrust orbital phasing maneuver
|
Shang, Haibin
|
|
2015
|
42 |
C |
p. 365-375
11 p.
|
artikel
|
| 12 |
Drag and heat reduction mechanism in the combinational opposing jet and acoustic cavity concept for hypersonic vehicles
|
Huang, Wei
|
|
2015
|
42 |
C |
p. 407-414
8 p.
|
artikel
|
| 13 |
Dynamic stability conditions for a rolling flight vehicle applying continuous actuator
|
Koohmaskan, Yousof
|
|
2015
|
42 |
C |
p. 451-458
8 p.
|
artikel
|
| 14 |
Editorial Board
|
|
|
2015
|
42 |
C |
p. IFC-
1 p.
|
artikel
|
| 15 |
Effect of aspect ratio on wing rock at low Reynolds number
|
Go, Tiauw Hiong
|
|
2015
|
42 |
C |
p. 267-273
7 p.
|
artikel
|
| 16 |
Evaluating military training aircrafts through the combination of multi-criteria decision making processes with fuzzy logic. A case study in the Spanish Air Force Academy
|
Sánchez-Lozano, J.M.
|
|
2015
|
42 |
C |
p. 58-65
8 p.
|
artikel
|
| 17 |
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor
|
Wang, Z.P.
|
|
2015
|
42 |
C |
p. 169-175
7 p.
|
artikel
|
| 18 |
Finite element analysis for acoustic characteristics of combustion stabilization devices
|
Kim, Seong-Ku
|
|
2015
|
42 |
C |
p. 229-240
12 p.
|
artikel
|
| 19 |
Generation of Richtmyer–Meshkov and secondary instabilities during the interaction of an energy release with a cylinder shock layer
|
Azarova, O.A.
|
|
2015
|
42 |
C |
p. 376-383
8 p.
|
artikel
|
| 20 |
Hierarchical modeling and optimization of camber morphing airfoil
|
Murugan, Senthil
|
|
2015
|
42 |
C |
p. 31-38
8 p.
|
artikel
|
| 21 |
Ignition theory investigation and experimental research on hybrid rocket motor
|
Tian, Hui
|
|
2015
|
42 |
C |
p. 334-341
8 p.
|
artikel
|
| 22 |
Integrated guidance and control law for cooperative attack of multiple missiles
|
Wang, Xiaofang
|
|
2015
|
42 |
C |
p. 1-11
11 p.
|
artikel
|
| 23 |
Linear and nonlinear control strategies for formation and station keeping of spacecrafts within the context of the three body problem
|
Darvish, Kourosh
|
|
2015
|
42 |
C |
p. 12-24
13 p.
|
artikel
|
| 24 |
Liquefying fuel regression rate modeling in hybrid propulsion
|
Lestrade, J.-Y.
|
|
2015
|
42 |
C |
p. 80-87
8 p.
|
artikel
|
| 25 |
Low frequency instability in laboratory-scale hybrid rocket motors
|
Park, Kyung-Su
|
|
2015
|
42 |
C |
p. 148-157
10 p.
|
artikel
|
| 26 |
Measured aerodynamic characteristics of wings at low Reynolds numbers
|
Ananda, G.K.
|
|
2015
|
42 |
C |
p. 392-406
15 p.
|
artikel
|
| 27 |
Modal behavior of a new large reflector conceptual design
|
Morterolle, Sébastien
|
|
2015
|
42 |
C |
p. 74-79
6 p.
|
artikel
|
| 28 |
Multi-fidelity optimization strategy for the industrial aerodynamic design of helicopter rotor blades
|
Leusink, Debbie
|
|
2015
|
42 |
C |
p. 136-147
12 p.
|
artikel
|
| 29 |
Nonlinear dynamics of a rotating triangular tethered satellite formation near libration points
|
Cai, Zhiqin
|
|
2015
|
42 |
C |
p. 384-391
8 p.
|
artikel
|
| 30 |
Novel approach for design of a waverider vehicle generated from axisymmetric supersonic flows past a pointed von Karman ogive
|
Ding, Feng
|
|
2015
|
42 |
C |
p. 297-308
12 p.
|
artikel
|
| 31 |
Numerical simulations and performance assessment of a scramjet powered cruise vehicle at Mach 8
|
Roncioni, Pietro
|
|
2015
|
42 |
C |
p. 218-228
11 p.
|
artikel
|
| 32 |
Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzles
|
Hadjadj, A.
|
|
2015
|
42 |
C |
p. 158-168
11 p.
|
artikel
|
| 33 |
Optimization and analysis of shock wave/boundary layer interaction for drag reduction by Shock Control Bump
|
Mazaheri, K.
|
|
2015
|
42 |
C |
p. 196-208
13 p.
|
artikel
|
| 34 |
Output feedback control of Lorentz-augmented spacecraft rendezvous
|
Huang, Xu
|
|
2015
|
42 |
C |
p. 241-248
8 p.
|
artikel
|
| 35 |
Positioning performance analysis using RWLS algorithm based on variance estimation methods
|
Mosavi, M.R.
|
|
2015
|
42 |
C |
p. 88-96
9 p.
|
artikel
|
| 36 |
Real-time estimation of helicopter blade kinematics using integrated linear displacement sensors
|
Allred, C. Jefferson
|
|
2015
|
42 |
C |
p. 274-286
13 p.
|
artikel
|
| 37 |
Regression rate and combustion performance investigation of aluminum metallized HTPB/98HP hybrid rocket motor with numerical simulation
|
Sun, Xingliang
|
|
2015
|
42 |
C |
p. 287-296
10 p.
|
artikel
|
| 38 |
Relative attitude and position estimation for a tumbling spacecraft
|
Zhang, Lijun
|
|
2015
|
42 |
C |
p. 97-105
9 p.
|
artikel
|
| 39 |
Rigid spacecraft attitude control using adaptive integral second order sliding mode
|
Tiwari, Pyare Mohan
|
|
2015
|
42 |
C |
p. 50-57
8 p.
|
artikel
|
| 40 |
Robust gain-scheduled autopilot design for spin-stabilized projectiles with a course-correction fuze
|
Theodoulis, Spilios
|
|
2015
|
42 |
C |
p. 477-489
13 p.
|
artikel
|
| 41 |
Robust gain scheduled control of spacecraft rendezvous system subject to input saturation
|
Wang, Qian
|
|
2015
|
42 |
C |
p. 442-450
9 p.
|
artikel
|
| 42 |
Robust multiple model adaptive estimation for spacecraft autonomous navigation
|
Xiong, K.
|
|
2015
|
42 |
C |
p. 249-258
10 p.
|
artikel
|
| 43 |
Simple finite-time attitude stabilization laws for rigid spacecraft with bounded inputs
|
Gui, Haichao
|
|
2015
|
42 |
C |
p. 176-186
11 p.
|
artikel
|
| 44 |
Simplified brain storm optimization approach to control parameter optimization in F/A-18 automatic carrier landing system
|
Li, Junnan
|
|
2015
|
42 |
C |
p. 187-195
9 p.
|
artikel
|
| 45 |
Specific force integration algorithm with high accuracy for strapdown inertial navigation system
|
Lin, Yurong
|
|
2015
|
42 |
C |
p. 25-30
6 p.
|
artikel
|
| 46 |
Switching robust control for a nanosatellite launch vehicle
|
Lu, Bei
|
|
2015
|
42 |
C |
p. 259-266
8 p.
|
artikel
|
| 47 |
The Adaptive Aspect Ratio morphing wing: Design concept and low fidelity skin optimization
|
Woods, Benjamin K.S.
|
|
2015
|
42 |
C |
p. 209-217
9 p.
|
artikel
|
| 48 |
Tracking control of spacecraft formation flying with collision avoidance
|
Hu, Qinglei
|
|
2015
|
42 |
C |
p. 353-364
12 p.
|
artikel
|
| 49 |
Variable geometry cowl sidewall for improving rectangular hypersonic inlet performance
|
Teng, Jian
|
|
2015
|
42 |
C |
p. 128-135
8 p.
|
artikel
|
| 50 |
Vibration tests on the preloaded LARES satellite and separation system
|
Paris, Claudio
|
|
2015
|
42 |
C |
p. 470-476
7 p.
|
artikel
|
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