nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A Convex Programming Approach to Mid-course Trajectory Optimization for Air-to-Ground Missiles
|
Kwon, Hyuck-Hoon |
|
|
21 |
2 |
p. 479-492 |
artikel |
2 |
Adaptive Differential Evolution-Based Distributed Model Predictive Control for Multi-UAV Formation Flight
|
Zhang, Boyang |
|
|
21 |
2 |
p. 538-548 |
artikel |
3 |
Adaptive Gliding-Guided Projectile Attitude Tracking Controller Design Based on RBF Neuro-sliding Mode Technique
|
Zhang, Wenguang |
|
|
21 |
2 |
p. 504-512 |
artikel |
4 |
Automatic Gain Tuning Method of a Quad-Rotor Geometric Attitude Controller Using A3C
|
Lee, Seongheon |
|
|
21 |
2 |
p. 469-478 |
artikel |
5 |
Change Detection in SAR Images Based on Deep Learning
|
Keshk, Hatem Magdy |
|
|
21 |
2 |
p. 549-559 |
artikel |
6 |
Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition
|
Wang, Ruixing |
|
|
21 |
2 |
p. 347-362 |
artikel |
7 |
Control Performance Analysis on Variable Configuration of Ducted-Fan Flight Array
|
Jeong, Junho |
|
|
21 |
2 |
p. 524-537 |
artikel |
8 |
CUSUM-based GNSS Spoofing Detection Method for Users of GNSS Augmentation System
|
Jeong, Seongkyun |
|
|
21 |
2 |
p. 513-523 |
artikel |
9 |
Development of Fault Detection and Identification Algorithm Using Deep learning for Nanosatellite Attitude Control System
|
Lee, Kwang-Hyun |
|
|
21 |
2 |
p. 576-585 |
artikel |
10 |
Dimensional Synthesis of Antenna-Deployable Support Structure
|
Lin, Fei |
|
|
21 |
2 |
p. 404-417 |
artikel |
11 |
Efficient Prediction of the Temperature History of a Hypersonic Vehicle Throughout the Mission Trajectory with an Aerodynamic Thermal Load Element
|
Kim, Gyubin |
|
|
21 |
2 |
p. 363-379 |
artikel |
12 |
Experimental Investigation of High-Angle-of-Attack Aerodynamics of Low-Aspect-Ratio Rectangular Wings Configured with NACA0012 Airfoil Section
|
Lee, Seok Ho |
|
|
21 |
2 |
p. 303-314 |
artikel |
13 |
Heat Flux and Pressure Reduction Using Aerospike and Counterflowing Jet on Complex Hypersonic Flow
|
Jia, Juhong |
|
|
21 |
2 |
p. 337-346 |
artikel |
14 |
L1 Penalized Sequential Convex Programming for Fast Trajectory Optimization: With Application to Optimal Missile Guidance
|
Roh, Heekun |
|
|
21 |
2 |
p. 493-503 |
artikel |
15 |
Multi-objective Optimization for Time-Open Lambert Rendezvous Between Non-coplanar Orbits
|
Wu, Guan-qun |
|
|
21 |
2 |
p. 560-575 |
artikel |
16 |
Numerical Analysis of Structural Soundness by Sloshing Movement in an External Fuel Tank for Rotorcraft
|
Kim, Sung Chan |
|
|
21 |
2 |
p. 380-393 |
artikel |
17 |
Numerical Study About Buffet Characteristics and Attenuation of Vertical Tail at High Angles of Attack
|
Kang, Dong Hun |
|
|
21 |
2 |
p. 315-328 |
artikel |
18 |
Present and Future of Air Navigation: PBN Operations and Supporting Technologies
|
López-Lago, Manuel |
|
|
21 |
2 |
p. 451-468 |
artikel |
19 |
Rotorcraft Comprehensive Analysis Calculations of a Coaxial Rotor with Lift Offset
|
Ho, Jimmy C. |
|
|
21 |
2 |
p. 418-438 |
artikel |
20 |
Stage Optimization of Anti-air Missiles Using Practical Guidance Laws
|
Hong, Seong-Min |
|
|
21 |
2 |
p. 394-403 |
artikel |
21 |
Study of Noise Reduction Based on Optimal Fan Outer Pressure Ratio and Thermodynamic Performance for Turbofan Engines at Conceptual Design Stage
|
Xue, Rui |
|
|
21 |
2 |
p. 439-450 |
artikel |
22 |
Three-Dimensional Shock-Wave/Boundary-Layer Interaction in Supersonic Flow Past a Finite-Span Sharp Wedge
|
Li, Weipeng |
|
|
21 |
2 |
p. 329-336 |
artikel |