no |
title |
author |
magazine |
year |
volume |
issue |
page(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 |
article |
2 |
A Cure for Numerical Instability of Discrete Adjoint Methods to Quasi-1D Flow Equations Near Boundaries
|
Kim, Minsoo |
|
|
22 |
6 |
p. 1302-1312 |
article |
3 |
Aeroacoustic Characteristic Analyses of Coaxial Rotors in Hover and Forward Flight
|
Wang, Bo |
|
|
22 |
6 |
p. 1278-1292 |
article |
4 |
A Parametric Study of the Functioning of an Axisymmetric Explosive Separation Device
|
Wang, Guangyu |
|
|
22 |
6 |
p. 1331-1343 |
article |
5 |
Application of Ground Flutter Emulation Test Technique for the Passive Flutter Suppression Effect Validation
|
Yun, Jong-Min |
|
|
22 |
6 |
p. 1344-1355 |
article |
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 |
article |
7 |
Closed-Form Impact-Angle-Control Guidance of Nose-Dive Missiles for Maximum Terminal Speed
|
Kim, Iksoo |
|
|
22 |
6 |
p. 1428-1439 |
article |
8 |
Correction to: A Practical Optimal Guidance Scheme Under Impact Angle and Terminal Acceleration Constraints
|
Chi, Hyo-Seon |
|
|
22 |
6 |
p. 1440-1441 |
article |
9 |
Design Sensitivity Analysis of Static Aeroelastic Stresses via Iterative Adjoint-Based Method
|
Cheng, Yunhe |
|
|
22 |
6 |
p. 1365-1382 |
article |
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 |
article |
11 |
GNSS Double Differences Used as Beacon Landing System for Aircraft Instrument Approach
|
Dautermann, Thomas |
|
|
22 |
6 |
p. 1455-1463 |
article |
12 |
Indirect Estimation Based Active Disturbance Rejection Control for Solar Sail Station-Keeping
|
Huang, Jia |
|
|
22 |
6 |
p. 1493-1503 |
article |
13 |
Numerical Investigation of a Ballistic Range Free Flight Model
|
Mahomed, I. |
|
|
22 |
6 |
p. 1293-1301 |
article |
14 |
Physics of Dynamic Stall Vortex During Pitching Oscillation of Dynamic Airfoil
|
Wei, Binbin |
|
|
22 |
6 |
p. 1263-1277 |
article |
15 |
Research on Calculation Method of Fuel Temperature According to Airworthiness Regulations
|
Zhang, Ruihua |
|
|
22 |
6 |
p. 1504-1511 |
article |
16 |
Satellite Imagery Super-Resolution Using Squeeze-and-Excitation-Based GAN
|
Moustafa, Marwa S. |
|
|
22 |
6 |
p. 1481-1492 |
article |
17 |
Selective Goal Aiming Rapidly Exploring Random Tree Path Planning for UAVs
|
Noh, Geemoon |
|
|
22 |
6 |
p. 1397-1412 |
article |
18 |
Spatial–Temporal Clustering and Optimization of Aircraft Descent and Approach Trajectories
|
Yang, Zhao |
|
|
22 |
6 |
p. 1512-1523 |
article |
19 |
The Design Improvement of a Rotary-Wing Aircraft Frame Considering Fatigue Life and Fracture Characteristics
|
Kim, Mantae |
|
|
22 |
6 |
p. 1313-1320 |
article |
20 |
The Optimization Process of Aircraft Side Panel’s Weight Reduction Based on Orthogonal Experiment
|
Chu, Jianjie |
|
|
22 |
6 |
p. 1321-1330 |
article |
21 |
UAV Formation Obstacle Avoidance Control Algorithm Based on Improved Artificial Potential Field and Consensus
|
Wang, Ning |
|
|
22 |
6 |
p. 1413-1427 |
article |
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 |
article |