no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
1 |
A brief review on in-orbit refueling projects and critical techniques
|
Malyh, Daria |
|
|
|
2 |
p. 185-196 |
article |
2 |
Acceleration control of a multi-rotor UAV towards achieving microgravity
|
Kedarisetty, Siddhardha |
|
|
|
2 |
p. 175-188 |
article |
3 |
Accident propensity assessment of Boeing 737 Aircraft variants using the Gompertz distribution model
|
Faiyetole, Ayodele Adekunle |
|
|
|
2 |
p. 259-283 |
article |
4 |
A combined configuration (αβ filter- TRIAD algorithm) for spacecraft attitude estimation based on in-Orbit Flight Data
|
Boussadia, Halima |
|
|
|
2 |
p. 223-232 |
article |
5 |
A discrete design method of repeat ground track orbit for Earth observation satellites
|
Wei, Xiaofang |
|
|
|
2 |
p. 199-206 |
article |
6 |
Aerial image detection and recognition system based on deep neural network
|
Zhang, Shizhao |
|
|
|
2 |
p. 101-108 |
article |
7 |
Aerothermal characteristics of transonic over-tip leakage flow for different tip geometries with cooling injection
|
Tang, Mingxing |
|
|
|
2 |
p. 189-196 |
article |
8 |
A method for flight test subject allocation on multiple test aircrafts based on improved genetic algorithm
|
Liu, Yibo |
|
|
|
2 |
p. 215-225 |
article |
9 |
Analysis of BDS GEO satellite multipath effect for GNSS integrity monitoring in civil aviation
|
Chang, Jin |
|
|
|
2 |
p. 133-141 |
article |
10 |
Analysis of error induced by the Doppler effect in the ROSI beamforming for rotating sound source identification
|
Wang, Yuxi |
|
|
|
2 |
p. 323-330 |
article |
11 |
An enhanced situational awareness design for airborne surveillance based on Automatic Dependent Surveillance–Broadcast
|
Zhao, Wenhao |
|
|
|
2 |
p. 109-118 |
article |
12 |
An optimal deployment method of heterogeneous sensors for multi-agent collaborative detection tasks
|
He, Yangguang |
|
|
|
2 |
p. 249-257 |
article |
13 |
A numerical study of the dynamic properties of Miura folded metamaterials
|
Zhang, Dapeng |
|
|
|
2 |
p. 125-135 |
article |
14 |
Application of mathematical modeling for certification of superjet-100 airplane
|
Pogosyan, M. A. |
|
|
|
2 |
p. 155-161 |
article |
15 |
Application of the dynamic programming method to ensure of dual-channel attitude control of an asymmetric spacecraft in a rarefied atmosphere of Mars
|
Bakry, Ibrahim |
|
|
|
2 |
p. 213-221 |
article |
16 |
A spatiotemporal transferable image fusion technique for GeoEye-1 satellite imagery
|
Elshora, Mohamed |
|
|
|
2 |
p. 305-322 |
article |
17 |
Backstepping sliding mode-based anti-skid braking control for a civil aircraft
|
Ma, Zhenjie |
|
|
|
2 |
p. 187-197 |
article |
18 |
Behavior of mixing enhancement in microscale shock cylindrical bubble interaction
|
Wang, Zi’ang |
|
|
|
2 |
p. 143-149 |
article |
19 |
Computational analyses of tail fin configurations for a sounding rocket
|
Sankalp, S. Sai |
|
|
|
2 |
p. 233-246 |
article |
20 |
Development of indoor folding method for tethered aerostat envelope to stow for long duration safely
|
Cheulkar, Avesh |
|
|
|
2 |
p. 301-307 |
article |
21 |
Dynamics and stabilization of flexible spacecraft structures with magnetic coil-pair actuators
|
Pawlina, Bryan |
|
|
|
2 |
p. 147-155 |
article |
22 |
Effect of elastic properties dependence of the stress state in composite materials
|
Fedorenko, A. N. |
|
|
|
2 |
p. 105-109 |
article |
23 |
Effect of nucleation and icing evolution on run-back freezing of supercooled water droplet
|
Sun, Mingming |
|
|
|
2 |
p. 147-153 |
article |
24 |
Effect of tip injection on the flow characteristics of an aeroengine compressor rotor
|
Li, Yidan |
|
|
|
2 |
p. 151-169 |
article |
25 |
Enhanced composite nonlinear extended state observer based on trajectory linearization control in presence of external and internal disturbance
|
Hosseinpour, Javid |
|
|
|
2 |
p. 353-364 |
article |
26 |
Error characteristics analysis and calibration testing for MEMS IMU gyroscope
|
Zhang, Pengyu |
|
|
|
2 |
p. 97-104 |
article |
27 |
Expediency of using moving-base flight simulators in research on pilot aids evaluation
|
Voronka, Tatyana |
|
|
|
2 |
p. 207-212 |
article |
28 |
Fault isolation of reaction wheels onboard three-axis controlled in-orbit satellite using ensemble machine learning
|
Rahimi, Afshin |
|
|
|
2 |
p. 119-126 |
article |
29 |
Filter and sensor delay synchronization in incremental flight control laws
|
Steffensen, Rasmus |
|
|
|
2 |
p. 285-304 |
article |
30 |
Frequent high-utility sequential pattern mining algorithm for integrated architecture design of multi-platform mission system
|
Ni, Xiang |
|
|
|
2 |
p. 331-347 |
article |
31 |
Fusion object detection of satellite imagery with arbitrary-oriented region convolutional neural network
|
Ya, Ying |
|
|
|
2 |
p. 163-174 |
article |
32 |
Harmonic balance analysis and simulations of spacecraft rendezvous and formation flying dynamics
|
Ogundele, Ayansola D. |
|
|
|
2 |
p. 119-132 |
article |
33 |
Improved multi-target tracking crossing paths in MIMO FMCW 8 × 16 radar system using a new hybrid AMC-JPDAF algorithm
|
Zarai, Khaireddine |
|
|
|
2 |
p. 343-351 |
article |
34 |
Increasing relative angular velocity for air combat in zero gravity
|
Deng, Bill |
|
|
|
2 |
p. 83-95 |
article |
35 |
Influence of non-uniform inflow swirl and hot streak on turbine vane
|
Zhang, Xiuhe |
|
|
|
2 |
p. 79-85 |
article |
36 |
In-orbit target tracking by flyby and formation-flying spacecraft
|
Hakima, Houman |
|
|
|
2 |
p. 197-212 |
article |
37 |
Intelligent sensing and control for aerospace unmanned systems
|
Li, Yuankai |
|
|
|
2 |
p. 167-169 |
article |
38 |
Joint image pansharpening and registration via structure tensor total variation regularization
|
Yuan, Yu |
|
|
|
2 |
p. 277-283 |
article |
39 |
LMI-based linear parameter varying PID control design and its application to an aircraft control system
|
Huang, Bixuan |
|
|
|
2 |
p. 309-321 |
article |
40 |
Method for predictive analysis of failure and pre-failure conditions of aircraft units using data obtained during their operation
|
Smagin, D. I. |
|
|
|
2 |
p. 231-248 |
article |
41 |
Modal equivalent method of full-area membrane and grid membrane
|
Zhang, Yibei |
|
2018 |
|
2 |
p. 129-137 |
article |
42 |
Modeling and simulation of a direct-ascent anti-satellite missile using Kerbal Space Program (KSP)
|
Kawthalkar, Apurva |
|
|
|
2 |
p. 285-299 |
article |
43 |
Modeling hybrid polymer–nanometal lightweight structures
|
Bhaga, Bharat |
|
|
|
2 |
p. 119-124 |
article |
44 |
Modeling of manufacturing of thermoplastic composites and residual stress prediction
|
Fedulov, B. N. |
|
2018 |
|
2 |
p. 81-86 |
article |
45 |
Modelling and simulation of the power subsystem of a low earth orbit CubeSat
|
Parthasarathy, Varsha |
|
|
|
2 |
p. 139-146 |
article |
46 |
Nonlinear optimal control for autonomous hypersonic vehicles
|
Rigatos, G. |
|
|
|
2 |
p. 197-213 |
article |
47 |
Nonlinear optimal controller design for nonlinear spacecraft formation flying with periodic coefficients via SDRE technique
|
Ogundele, Ayansola D. |
|
|
|
2 |
p. 247-263 |
article |
48 |
Numerical and experimental investigations of compressed stiffened composite panel with local impact damage
|
Ryabov, A. A. |
|
2018 |
|
2 |
p. 99-107 |
article |
49 |
Numerical investigation on aircraft wing stiffener composite material integration
|
Doggui, Mohamed Montassar |
|
|
|
2 |
p. 137-145 |
article |
50 |
Observer design for linear models of multi-rate asynchronous aerospace systems
|
Moarref, Miad |
|
|
|
2 |
p. 127-137 |
article |
51 |
On aeroelastic response of an airfoil under dynamic stall using time delay neural network
|
Qiu, Zhan |
|
2018 |
|
2 |
p. 87-97 |
article |
52 |
Optimization of vertical stabilizer structure diagram
|
Erik, Tytaev |
|
|
|
2 |
p. 97-105 |
article |
53 |
Orbit–attitude dynamics and control of spacecraft hovering over a captured asteroid in the earth–moon system
|
Fu, Jiangliang |
|
|
|
2 |
p. 265-275 |
article |
54 |
Phased microphone array for sound source localization with deep learning
|
Ma, Wei |
|
|
|
2 |
p. 71-81 |
article |
55 |
Recent developments of blended wing body aircraft: experimental, numerical and theoretical approaches
|
Handa, Sanyam |
|
|
|
2 |
p. 171-183 |
article |
56 |
Recursive optimal linear attitude estimator based on star sensor and gyro
|
Xu, Guangtan |
|
|
|
2 |
p. 91-99 |
article |
57 |
Reliability evaluation method of complex technical systems based on test results of disassembled components
|
Amosov, Alexey |
|
|
|
2 |
p. 335-342 |
article |
58 |
Reliable and improved selection of fins/trim tabs layouts on rocket to control the direct flight
|
Nadjafi, Mohammad |
|
|
|
2 |
p. 213-230 |
article |
59 |
Research on refraction error correction of digital image correlation technology in strain measurement of airship skin
|
Zhao, Liuyue |
|
|
|
2 |
p. 107-117 |
article |
60 |
Research on route planning based on performance constraints for UAS in battlefield
|
Liu, Bowen |
|
2018 |
|
2 |
p. 73-80 |
article |
61 |
Reynolds number influence on the backpressure-induced shock–boundary layer interaction in an asymmetric supersonic expansion flow
|
Ji, Yuan |
|
|
|
2 |
p. 111-118 |
article |
62 |
Robot grasp detection based on key point estimation
|
Li, Yulong |
|
|
|
2 |
p. 323-333 |
article |
63 |
State estimation of radar tracking system using a robust adaptive unscented Kalman filter
|
Kumar, Manav |
|
|
|
2 |
p. 375-381 |
article |
64 |
Structural design and optimization of a morphing wing trailing edge flap
|
Ding, Shuai |
|
2018 |
|
2 |
p. 109-119 |
article |
65 |
Substantiation of choosing rational appearance of nose of aircraft with the use of mathematical modeling
|
Barabanov, A. V. |
|
|
|
2 |
p. 171-177 |
article |
66 |
Supersonic cruise flight of Vth generation fighters
|
Bashkirov, I. |
|
2018 |
|
2 |
p. 121-127 |
article |
67 |
The numerical simulation of fatigue crack propagation in Inconel 718 alloy at different temperatures
|
Duan, Chi |
|
|
|
2 |
p. 87-95 |
article |
68 |
Three-axis high-accuracy spacecraft attitude estimation via sequential extended Kalman filtering of single-axis magnetometer measurements
|
Habib, Tamer Mekky Ahmed |
|
|
|
2 |
p. 365-374 |
article |