This proceedings book focuses on the theme of "Space in Future," discusses related topics of space development, and further promotes international cooperation. The 10th CSA-IAA Conference on Advanced Space Technology attracts about 300 space professionals from home and abroad.
The book mainly covers six topics: Development and prospect in deep space exploration; directions of space transportation in future; new trends, breakthroughs of satellite and its applications; future direction of guidance, navigation, and control; breakthrough technology in space power system; and new mode of cooperation for future space development.
This book helps to establish a platform of academic exchange for space professionals all over the world, offer suggestions of sustainable development of space technology and space industry, and further expand the depth and breadth of space international academic exchange and cooperation.
Mission Planning for Agile Earth-Observing Satellites towards the Best
Reactivity.- Study on the Attitude Control Scheme of Yaw Steering with Front
and Back Pointing to the Sun Alternately.- Integration Thrust Regulation
Technology of Variable-Thrust Liquid Rocket EngineTechnology for
Next-Generation Launch Vehicle.- Adaptive fault-tolerant control for space
robot manipulators via online fault estimation.- Orbital motion of Lorentz
spacecraft during the low-energy Jupiter flyby.- Design and development of
intelligent nitrogen charging device based on barrel bomb maintenance.-
Attitude and Orbit Coupling Control of GEO satellites Using Electric
Propulsion with Mechanical Arm.- Lunar dust removal technology based on
high-voltage electrostatic field.- Actuator layout optimization for active
vibration control of rigid-flexible spacecraft using genetic algorithm.- A
Novel Method to Construct Electrochemical Model for the Lithium-Ion Battery
Using Less Prior Knowledge.- Design and Output Force Optimization of a New
Hybrid Actuator.- Design of automatic light adjustment algorithm for space
camera based on improved Zero-DCE.- Data-driving method of real-time state
estimation with multiple periods.- A Low-cost On-orbit Propellant Supply
System.- The Status and Development Proposal of China's Comprehensive
Environmental Observation Satellites System.- Design characteristics and
manufacture practice of micro satellites.- A narrow band wireless network
applied for NANO-satellites cluster.- Design of whole process virtual test
system for structural thermal test of aerospace structures.- Module partition
of satellite platform based on weighted complex networks.- Experimental study
on the working process of kerosene gel rocket motor.- Research on
Multi-Damage Self-Identification Method for Reusable Aerospace Composite
Structure.- Numerical investigation on the influence of adhesion defects on
the mechanical properties of single lap joints.- Numerical study of
influencing effects on SRM nozzle damping coefficient.- Design and Analysis
of High-Precision High-Stability Thermal Control System of a Time-Frequency
Payload Under Complex Space Thermal Environment.- High-resolution monitoring
of near-surface methane concentration anomalies by AHSI payload of GF-5
satellite.- Event-triggered orbital cooperative control for the micro-nano
satellite cluster.- Lunar Dust Effects and Its Mitigation Methods.-
Contribution of two flexible structures to the thermal stability of
reflective star sensors.- Thermal control design and analysis of miniaturized
laser communication terminal in Medium Orbit.- Autonomous flight control
technology for Jupiter and beyond Deep space missions.- Digital Twin Modeling
of Hypersonic Flight Vehicles Based on Dynamic Regression Neural Network.-
Ice Giant Exploration Trajectory Design as A Secondary Payload in The
Heliopause Exploration Mission.- Progress on thermal control technology
development of space nuclear power.- Research on the Lifetime and Reliability
Assessment Techniques of Solar Arrays.- Analysis of the Impact of Flexible
Transmission Cables on Non-Contact Spacecraft Isolation Platforms.-
Low-Thrust Earth-Moon Transfer Trajectories Design with Sequential Convex
Optimization in Three-Body Systems.- Research on droplets collisions between
emission surface and extractor in the Ultrasonic Electric Propulsion system.-
Research on Control Technology of Reusable Lunar Surface Spacecraft.- Optical
meansurement and autonomous navigation technology for Tianwen-1
interplanetary flight.- Design of Libration Point Configuration for Space
Gravitational Wave Detection.- Research on the Propellant Utilization System
of Liquid Launch Vehicles.- Software Security Boot Design Based on
FMQL45-T900 Platform.- Six-Degree-of-Freedom Physical Simulation System
Design of Spacecraft.- HWIL System Based on Dome-Screen Projector for
On-Orbit Servicing GNCS.- Analysis of Low-Cost Pathways for "Satellite
Express".- NY GNSS reflection measurements: task review and preliminary
results.- System Architecture Design of Multi-satellite Coordination
Autonomous Mission Planning.- A table driven plug-in design method for Launch
vehicle ground test software communication interface.- An electro hydraulic
servo fault diagnosis method based on BP optimized by GA and LM, GRU and RF.-
Micro-vibration analysis of satellite structures under mechanical and thermal
coupling.- Bibliometric Study of China's International Cooperation in
Astronautics Research.- Intelligent Compressed Spectrum Hole Detection in
Anti-jamming Satellite Communications .- Predictor-corrector Guidance for
Hypersonic Morphing Vehicle.- Microstructure and tensile properties evolution
of Mg-Gd-Y alloy during metal additive forging process.- Thrust Evaluation of
the Rotating Magnetic Sail by Three-Dimensional Particle Tracing Analysis.-
Atmospheric Neutron Inversion Model Based on Backpropagation Neural Network.-
A Method for Calculating Illumination at Different Heights of in the Lunar
South Pole Region and Its Application in Site Selection.- Dynamics analysis
and control of a large flexible net and multi-star systems for
non-cooperative targets.- Design and Application of Adaptive Interface Plugin
for Launch Vehicle Test Software based on Qt.- CPU-GPU coupling
optimizations in the context of a GPU machine cluster for cuBLAS.- The
Promise and Challenge of Deploying Safe Artificial Intelligence on Manned
Planetary Exploration Rover.- Numerical study of soft PSD deformation in
pulse solid rocket motor based on peridynamics.- Research on Multi-Receiver
Spoofing Detection Algorithm.
The Chinese Society of Astronautics (CSA) was founded in October 1979. Composed of space science and technology professionals, CSA is an NGO with the most academic representation and international influence in China's space community. CSA aims to promote innovation and development of space science and technology and facilitate its popularization and dissemination. CSA has 47 committees, more than 200 institutional members, and 100,000 individual members, and has joint offices with the branches of two international organizations, namely the Studies Center of the International Academy of Astronautics (IAA) and the Select Sub-Committee on Satellite Commercial Applications (IAF).
Shanghai Academy of Spaceflight Technology (SAST) is a member of China Aerospace Science and Technology Corporation (CASC) and comprises 21 affiliated companies. It is one of the largest suppliers of advanced aerospace technology and air defense products in China. SAST has made significant contributions to the aerospace industry of China by taking a key role in the R&D of launch vehicles, satellites, spacecrafts, deep exploration, air defense, etc. SAST is equipped with distinguished technologies in system engineering, space propulsion, guidance navigation and control (GNC), space power source, structure material, etc. In addition, the core technologies are merged with civil applications. As a result, spin-off industries are formed in vehicle lithium batteries, natural gas transmission and distribution, mechatronic equipment, composite materials, etc.
