| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A study on the high stability control for the integrated aero-propulsion system under supersonic state
|
Sun, Fengyong
|
|
|
76 |
C |
p. 350-360
|
artikel
|
| 2 |
Attitude stabilization of flapping micro-air vehicles via an observer-based sliding mode control method
|
Tran, Xuan-Toa
|
|
|
76 |
C |
p. 386-393
|
artikel
|
| 3 |
A turboshaft engine NMPC scheme for helicopter autorotation recovery maneuver
|
Zheng, Qiangang
|
|
|
76 |
C |
p. 421-432
|
artikel
|
| 4 |
Casing grooves to improve aerodynamic performance of a HP turbine blade
|
Kavurmacioglu, Levent Ali
|
|
|
76 |
C |
p. 194-203
|
artikel
|
| 5 |
Centralized predictive ceiling interaction control of quadrotor VTOL UAV
|
Kocer, Basaran Bahadir
|
|
|
76 |
C |
p. 455-465
|
artikel
|
| 6 |
Combined high-speed and high-lift wing aerodynamic optimization using a coupled VLM-2.5D RANS approach
|
Parenteau, M.
|
|
|
76 |
C |
p. 484-496
|
artikel
|
| 7 |
Computational guidance for planetary powered descent using collaborative optimization
|
Jiang, Xiuqiang
|
|
|
76 |
C |
p. 37-48
|
artikel
|
| 8 |
Control-relevant modeling and performance limitation analysis for flexible air-breathing hypersonic vehicles
|
Shen, Haidong
|
|
|
76 |
C |
p. 340-349
|
artikel
|
| 9 |
Cooperative circular pattern target tracking using navigation function
|
Hong, Jinsung
|
|
|
76 |
C |
p. 105-111
|
artikel
|
| 10 |
Cooperative multiple task assignment problem with stochastic velocities and time windows for heterogeneous unmanned aerial vehicles using a genetic algorithm
|
Jia, Zhenyue
|
|
|
76 |
C |
p. 112-125
|
artikel
|
| 11 |
Cooperative search-attack mission planning for multi-UAV based on intelligent self-organized algorithm
|
Zhen, Ziyang
|
|
|
76 |
C |
p. 402-411
|
artikel
|
| 12 |
Design and investigation on variable Mach number waverider for a wide-speed range
|
Li, Shibin
|
|
|
76 |
C |
p. 291-302
|
artikel
|
| 13 |
Designing a closed-loop guidance system to increase the accuracy of satellite-carrier boosters' landing point
|
Tavakoli, Farhad
|
|
|
76 |
C |
p. 242-249
|
artikel
|
| 14 |
Design optimization of the last stage of a 4.5-stage compressor using a POD-based hybrid model
|
Luo, Jiaqi
|
|
|
76 |
C |
p. 303-314
|
artikel
|
| 15 |
Drag reduction investigation for hypersonic lifting-body vehicles with aerospike and long penetration mode counterflowing jet
|
Deng, Fan
|
|
|
76 |
C |
p. 361-373
|
artikel
|
| 16 |
Editorial Board
|
|
|
|
76 |
C |
p. ii
|
artikel
|
| 17 |
Effect of continuous Mach number variation of incoming flow on ram–scram transition in a dual-mode combustor
|
Zhang, Chenlin
|
|
|
76 |
C |
p. 433-441
|
artikel
|
| 18 |
Effect of strut length on combustion performance of a trapped vortex combustor
|
Li, Mingyu
|
|
|
76 |
C |
p. 204-216
|
artikel
|
| 19 |
Efficient aeroelastic reduced order model with global structural modifications
|
Chen, Gang
|
|
|
76 |
C |
p. 1-13
|
artikel
|
| 20 |
Evaluation and selection of missile's optimal initial launch azimuth under side window detection using a hybrid decision making method
|
Yu, Ying
|
|
|
76 |
C |
p. 217-228
|
artikel
|
| 21 |
Formation flight of unmanned aerial vehicles using track guidance
|
Lee, Dongwoo
|
|
|
76 |
C |
p. 412-420
|
artikel
|
| 22 |
Image-based attitude maneuvers for space debris tracking
|
Felicetti, Leonard
|
|
|
76 |
C |
p. 58-71
|
artikel
|
| 23 |
Improved Kriging with extremum response surface method for structural dynamic reliability and sensitivity analyses
|
Lu, Cheng
|
|
|
76 |
C |
p. 164-175
|
artikel
|
| 24 |
Influence of repetitive laser pulse energy depositions on supersonic flow over a sphere, cone and oblate spheroid
|
Rezaei Sangtabi, Ahmad
|
|
|
76 |
C |
p. 72-81
|
artikel
|
| 25 |
Local and global flame characteristics in a liquid kerosene fueled supersonic combustor equipped with a thin strut
|
Zhang, Junlong
|
|
|
76 |
C |
p. 49-57
|
artikel
|
| 26 |
Mixed adaptive control architecture for a novel coaxial-ducted-fan aircraft under time-varying uncertainties
|
Fan, Wei
|
|
|
76 |
C |
p. 141-154
|
artikel
|
| 27 |
Multi-constrained ascent guidance for solid propellant launch vehicles
|
Xu, Zhi
|
|
|
76 |
C |
p. 260-271
|
artikel
|
| 28 |
Multidimensional material response simulations of a full-scale tiled ablative heatshield
|
Meurisse, Jeremie B.E.
|
|
|
76 |
C |
p. 497-511
|
artikel
|
| 29 |
Near time-optimal feedback instantaneous impact point (IIP) guidance law for rocket
|
Jo, Byeong-Un
|
|
|
76 |
C |
p. 523-529
|
artikel
|
| 30 |
Nonlinear disturbance observer-based robust control for spacecraft formation flying
|
Lee, Daero
|
|
|
76 |
C |
p. 82-90
|
artikel
|
| 31 |
Nonlinear Kalman filters for aircraft engine gas path health estimation with measurement uncertainty
|
Lu, Feng
|
|
|
76 |
C |
p. 126-140
|
artikel
|
| 32 |
Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS)
|
Eshghi, Samira
|
|
|
76 |
C |
p. 14-26
|
artikel
|
| 33 |
Recursive decentralized control for robotic manipulators
|
Hu, Quan
|
|
|
76 |
C |
p. 374-385
|
artikel
|
| 34 |
Robust and global attitude stabilization of magnetically actuated spacecraft through sliding mode
|
Sofyalı, Ahmet
|
|
|
76 |
C |
p. 91-104
|
artikel
|
| 35 |
Roll performance assessment of a light aircraft: Flight simulations and flight tests
|
Nicolosi, Fabrizio
|
|
|
76 |
C |
p. 471-483
|
artikel
|
| 36 |
Separation control by a microfabricated SDBD plasma actuator for small engine turbine applications: influence of the excitation waveform
|
Pescini, E.
|
|
|
76 |
C |
p. 442-454
|
artikel
|
| 37 |
Sequential convex programming for nonlinear optimal control problems in UAV path planning
|
Zhang, Zhe
|
|
|
76 |
C |
p. 280-290
|
artikel
|
| 38 |
Shape memory alloy-based mechanism for aeronautical application: Theory, optimization and experiment
|
Leal, Pedro B.C.
|
|
|
76 |
C |
p. 155-163
|
artikel
|
| 39 |
Static analysis of non-uniform 2D functionally graded auxetic-porous circular plates interacting with the gradient elastic foundations involving friction force
|
Behravan Rad, A.
|
|
|
76 |
C |
p. 315-339
|
artikel
|
| 40 |
Station keeping and momentum management of low-thrust satellites using MPC
|
Weiss, Avishai
|
|
|
76 |
C |
p. 229-241
|
artikel
|
| 41 |
Stochastic gradient particle swarm optimization based entry trajectory rapid planning for hypersonic glide vehicles
|
Li, Zhenhua
|
|
|
76 |
C |
p. 176-186
|
artikel
|
| 42 |
Stress distribution analysis and optimization for composite laminate containing hole of different shapes
|
Su, Zixing
|
|
|
76 |
C |
p. 466-470
|
artikel
|
| 43 |
The effect of pressure and oxygen concentration on the ignition and combustion of aluminum–magnesium fuel-rich propellant
|
Li, Lian-bo
|
|
|
76 |
C |
p. 394-401
|
artikel
|
| 44 |
The impact of casing groove location on the flow instability in a counter-rotating axial flow compressor
|
Mao, Xiaochen
|
|
|
76 |
C |
p. 250-259
|
artikel
|
| 45 |
The influence of micro air jets on mixing augmentation of fuel in cavity flameholder at supersonic flow
|
Fallah, Keivan
|
|
|
76 |
C |
p. 187-193
|
artikel
|
| 46 |
The solar-tracking optimal trajectory planning research based on minimum energy consumption in SSPS
|
Jin, Qi-Bao
|
|
|
76 |
C |
p. 272-279
|
artikel
|
| 47 |
The Transformer aircraft: A multimission unmanned aerial vehicle capable of symmetric and asymmetric span morphing
|
Ajaj, Rafic M.
|
|
|
76 |
C |
p. 512-522
|
artikel
|
| 48 |
Unsteady simulation and experimental study of hydrogen peroxide throttleable catalyst hybrid rocket motor
|
Zhao, Bo
|
|
|
76 |
C |
p. 27-36
|
artikel
|
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