The International Journal of Aeronautical and Space Sciences (IJASS) encourages submission of papers addressing all aspects of aerospace science and technology, which include acoustics, aerodynamics and fluid mechanics, aerospace telecommunications, airworthiness and maintenance, avionics, combustion and propulsion, flight dynamics, guidance and control, flight simulation and operations, low carbon manufacturing, nano application, plasmas and lasers, research instrumentation and facilities, space exploration, structural dynamics and aeroelasticity, structures and materials, and thermomechanics and reacting flows. The journal also addresses the ground and flight tests of aerospace systems including aircraft, air ship, helicopter, microelectromechanical system, missile, satellite, rocket, and UAV.
《国际航空与空间科学杂志》 (IJASS)鼓励提交涉及航空航天科学和技术各个方面的论文，包括声学，空气动力学和流体力学，航空电信，适航性和维护，航空电子设备，燃烧和推进，飞行动力学，制导和控制，飞行模拟和操作，低碳制造，纳米应用，等离子体和激光，研究仪器和设施，空间探索，结构动力学和空气弹性，结构和材料，热机械和反应流。该杂志还介绍了航空航天系统的地面和飞行测试，包括飞机，航空飞船，直升机，微机电系统，导弹，卫星，火箭和无人机。
Robust Concrete Crack Detection Using Deep Learning-Based Semantic Segmentation
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0120-5
Vision-Based Tracking of a Ground-Moving Target with UAV
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00142-Z
Evaluation System for Ablative Material in a High-Temperature Torch
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00185-2
Attitude Maneuver of Dual Rigid Bodies Spacecraft Using hp-Adaptive Pseudo-spectral Method
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0127-Y
Aeroelastic Stability Analysis of Curved Composite Blades in Hover Using Fully Intrinsic Equations
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00161-W
Flexible Design of Dual-Band Radar-Absorbing Composites by Controllable Permittivity
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00143-Y
A Traveling Salesman Problem-Based Approach to Observation Scheduling for Satellite Constellation
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00151-Y
Free Vibration Analysis of Graphene Platelets–Reinforced Composites Plates in Thermal Environment Based on Higher-Order Shear Deformation Plate Theory
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00184-3
Augmented Polynomial Guidance with Terminal Speed Constraints for Unpowered Aerial Vehicles
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0093-4
Time-Varying Formation Tracking for Multiple UAVs with Nonholonomic Constraints and Input Quantization via Adaptive Backstepping Control
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00157-6
An Evaluation Method of Combat Aircraft Contribution Effectiveness Based on Mission Success Space Design
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0111-6
Performance Analysis on Transmission Estimation for Avionics Real-Time System Using Optimized Network Calculus
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-00140-7
Layout Optimization for Blended Wing Body Aircraft Structure
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00172-7
Aeroelastic Study for HART II Rotor Using Unstructured Mixed Meshes
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0119-Y
Experimental Studies on Micro-Vortex Generator Controlled Shock/Boundary-Layer Interactions in Mach 2.2 Intake
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00166-5
Vision-Based Relative Navigation Using Dual Quaternion for Spacecraft Proximity Operations
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00171-8
The Effects of Wing Mass Asymmetry on Low-Speed Flight Characteristics of an Insect Model
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00165-6
Shape Optimization and Sensitivity Analysis of a Morphing-Wing Aircraft
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0110-7
Spacecraft Attitude Control Compensating Internal Payload Motion Using Disturbance Observer Technique
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0125-0
Hardware Implementation of KLT Tracker for Real-Time Intruder Detection and Tracking Using On-board Camera
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0131-2
Attitude Control of Underactuated and Momentum-Biased Satellite Using State-Dependent Riccati Equation Method
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0104-5
Investigation on the Dynamic Response of a Wide-Chord Fan Blade Under Ground Vortex Ingestion
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00150-Z
Effect of Inlet Boundary Layer Suction on Flow Distortion in Subsonic Diffusing S-Duct
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00175-4
Mach Number Determination in a High-Enthalpy Supersonic Arc-Heated Plasma Wind Tunnel
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0128-X
Optimization of the Spanwise Twist of a Flapping Wing for Bird-sized Aircraft using a Quasi-Steady Aerodynamic Model
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00154-9
Aerodynamic Analyses on the Steady and Unsteady Loading-Noise Sources of Drone Propellers
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00176-3
Tracking Control of Hypersonic Vehicles with Input Saturation Based on Fast Terminal Sliding Mode
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0109-0
Design of Synchronization Controller for the Station-Keeping Hovering Mode of Quad-Rotor Unmanned Aerial Vehicles
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0115-2
Computational Study on the Steady Loading Noise of Drone Propellers: Noise Source Modeling with the Lattice Boltzmann Method
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/s42405-019-00177-2
Improvement of DOD/DOA Estimation for Bistatic MIMO Radar
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00173-6
Numerical Simulation of Horizontal Axis Wind Turbines with Vortex Generators
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0118-Z
Static Shape Adjustment and Actuator Layered Optimization for Planar Phased Array Satellite Antenna
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00178-1
Development of General-Purpose Root-Finding Module for General Mission Analysis Tool
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0122-3
Hydraulic Characteristics of Liquid Film Generated by Slit Injector
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00167-4
Mistuning Effects on Aero-elastic Stability of Contra-Rotating Turbine Blades
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0108-1
A Numerical Study on the Effect of the Umbilical Plate on Longitudinal Controllability of a Low Aspect Ratio Launch Vehicle
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00196-Z
Development and Flight Test of Affordable Scientific Balloon System Suitable for Sea Recovery
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/s42405-019-00181-6
Performance Evaluation of a Rake Used for Measuring Total Pressure and Total Temperature Inside an Engine Inlet Duct
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00153-W
Infinite Horizon Optimal Output Feedback Control for Linear Systems with State Equality Constraints
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00145-W
Onboard Target Searching Strategy During Lost in Space Situations in Angles-Only Navigation Active Space Debris Removal
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00163-8
A Numerical Study on Flow-Through Model Design Considering the Internal Loss
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/s42405-019-00186-1
Supersonic Dual Bell Axisymmetric Minimum Length Nozzle Conception for High Propulsion Thrust
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00164-7
An Efficient Power-On Base Pressure Prediction Inside the Tube Using Axisymmetric and Quasi-Steady Computation
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00169-2
Cooperative sUAV Collision Avoidance Based on Satisficing Theory
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/s42405-019-00183-4
Attitude Control of Momentum-Biased Satellites Equipped with Control Moment Gyroscopes
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00194-1
Numerical Modeling of Pulsed Plasma Thruster Performance with Teflon Ablation and Ionization
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-00139-0
A New Collision Control Guidance Law Based on Speed Control for Kill Vehicles
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00147-8
Fuel Quantity Estimation of Aircraft Supplementary Tank Using Markov Chain Monte Carlo Method
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-019-00190-5
Computational Investigation on Unsteady Loads of High-Speed Rigid Coaxial Rotor with High-Efficient Trim Model
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/S42405-018-0133-0
Flight Performance Optimization Considering Environmental Impact Under Multi-RTA Constraints
来源期刊：International Journal of Aeronautical and Space SciencesDOI：10.1007/s42405-019-00179-0
