| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A Comparative Study of Hypervelocity Impact Characteristics in Aluminum Whipple Shielding Through 3D Measurement and Numerical Analysis
|
Park, Yurim
|
|
|
22 |
6 |
p. 1356-1364
|
artikel
|
| 2 |
A Cure for Numerical Instability of Discrete Adjoint Methods to Quasi-1D Flow Equations Near Boundaries
|
Kim, Minsoo
|
|
|
22 |
6 |
p. 1302-1312
|
artikel
|
| 3 |
Aeroacoustic Characteristic Analyses of Coaxial Rotors in Hover and Forward Flight
|
Wang, Bo
|
|
|
22 |
6 |
p. 1278-1292
|
artikel
|
| 4 |
A Parametric Study of the Functioning of an Axisymmetric Explosive Separation Device
|
Wang, Guangyu
|
|
|
22 |
6 |
p. 1331-1343
|
artikel
|
| 5 |
Application of Ground Flutter Emulation Test Technique for the Passive Flutter Suppression Effect Validation
|
Yun, Jong-Min
|
|
|
22 |
6 |
p. 1344-1355
|
artikel
|
| 6 |
Application of Neural Network Based on Real-Time Recursive Learning and Kalman Filter in Flight Data Identification
|
Li, Yao
|
|
|
22 |
6 |
p. 1383-1396
|
artikel
|
| 7 |
Closed-Form Impact-Angle-Control Guidance of Nose-Dive Missiles for Maximum Terminal Speed
|
Kim, Iksoo
|
|
|
22 |
6 |
p. 1428-1439
|
artikel
|
| 8 |
Correction to: A Practical Optimal Guidance Scheme Under Impact Angle and Terminal Acceleration Constraints
|
Chi, Hyo-Seon
|
|
|
22 |
6 |
p. 1440-1441
|
artikel
|
| 9 |
Design Sensitivity Analysis of Static Aeroelastic Stresses via Iterative Adjoint-Based Method
|
Cheng, Yunhe
|
|
|
22 |
6 |
p. 1365-1382
|
artikel
|
| 10 |
Development of Power Plant Trio CanSat Platform Powered by Solar, Wind and Piezo Energy Harvesting Systems
|
Chae, Bong-Geon
|
|
|
22 |
6 |
p. 1464-1480
|
artikel
|
| 11 |
GNSS Double Differences Used as Beacon Landing System for Aircraft Instrument Approach
|
Dautermann, Thomas
|
|
|
22 |
6 |
p. 1455-1463
|
artikel
|
| 12 |
Indirect Estimation Based Active Disturbance Rejection Control for Solar Sail Station-Keeping
|
Huang, Jia
|
|
|
22 |
6 |
p. 1493-1503
|
artikel
|
| 13 |
Numerical Investigation of a Ballistic Range Free Flight Model
|
Mahomed, I.
|
|
|
22 |
6 |
p. 1293-1301
|
artikel
|
| 14 |
Physics of Dynamic Stall Vortex During Pitching Oscillation of Dynamic Airfoil
|
Wei, Binbin
|
|
|
22 |
6 |
p. 1263-1277
|
artikel
|
| 15 |
Research on Calculation Method of Fuel Temperature According to Airworthiness Regulations
|
Zhang, Ruihua
|
|
|
22 |
6 |
p. 1504-1511
|
artikel
|
| 16 |
Satellite Imagery Super-Resolution Using Squeeze-and-Excitation-Based GAN
|
Moustafa, Marwa S.
|
|
|
22 |
6 |
p. 1481-1492
|
artikel
|
| 17 |
Selective Goal Aiming Rapidly Exploring Random Tree Path Planning for UAVs
|
Noh, Geemoon
|
|
|
22 |
6 |
p. 1397-1412
|
artikel
|
| 18 |
Spatial–Temporal Clustering and Optimization of Aircraft Descent and Approach Trajectories
|
Yang, Zhao
|
|
|
22 |
6 |
p. 1512-1523
|
artikel
|
| 19 |
The Design Improvement of a Rotary-Wing Aircraft Frame Considering Fatigue Life and Fracture Characteristics
|
Kim, Mantae
|
|
|
22 |
6 |
p. 1313-1320
|
artikel
|
| 20 |
The Optimization Process of Aircraft Side Panel’s Weight Reduction Based on Orthogonal Experiment
|
Chu, Jianjie
|
|
|
22 |
6 |
p. 1321-1330
|
artikel
|
| 21 |
UAV Formation Obstacle Avoidance Control Algorithm Based on Improved Artificial Potential Field and Consensus
|
Wang, Ning
|
|
|
22 |
6 |
p. 1413-1427
|
artikel
|
| 22 |
UDE-Based Robust Optimal Autopilot Design for Gliding-Guided Projectiles Subjected to Coupling Input Magnitude and Rate Saturation
|
Zhang, Wenguang
|
|
|
22 |
6 |
p. 1442-1454
|
artikel
|
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