Zong-Fu Luo

ORCID: 0000-0003-4871-4216
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About
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Research Areas
  • Spacecraft Dynamics and Control
  • Astro and Planetary Science
  • Space Satellite Systems and Control
  • Aerospace Engineering and Control Systems
  • Stellar, planetary, and galactic studies
  • Network Security and Intrusion Detection
  • IoT and Edge/Fog Computing
  • Anomaly Detection Techniques and Applications
  • Robotic Path Planning Algorithms
  • Guidance and Control Systems
  • Smart Grid Security and Resilience
  • Satellite Communication Systems
  • UAV Applications and Optimization
  • Solar and Space Plasma Dynamics
  • Advanced Malware Detection Techniques
  • Vehicle emissions and performance
  • Systems Engineering Methodologies and Applications
  • Complex Systems and Decision Making
  • Air Quality and Health Impacts
  • Modular Robots and Swarm Intelligence
  • Opportunistic and Delay-Tolerant Networks
  • Distributed Control Multi-Agent Systems
  • Air Traffic Management and Optimization
  • Soft Robotics and Applications
  • Space Science and Extraterrestrial Life

Sun Yat-sen University
2022-2024

Nanjing University
2020-2021

National University of Defense Technology
2010-2016

Naval Aeronautical and Astronautical University
2015-2016

10.1016/j.asr.2015.05.042 article EN Advances in Space Research 2015-06-07

10.1016/j.cnsns.2016.12.021 article EN Communications in Nonlinear Science and Numerical Simulation 2016-12-22

10.1007/s11431-010-3016-6 article EN Science China Technological Sciences 2010-07-14

10.2514/1.g000441 article EN Journal of Guidance Control and Dynamics 2014-06-20

ABSTRACT A massless particle can be naturally captured by a celestial body with the aid of third body. In this work, influence mass ratio on ballistic capture is investigated in planar circular restricted three-body problem (CR3BP) model. Four typical dynamical environments decreasing ratios, that is, Pluto–Charon, Earth–Moon, Sun–Jupiter, and Saturn–Titan systems, are considered. generalized method introduced to derive orbits starting from set initial conditions integrating backward time....

10.1093/mnras/staa2366 article EN Monthly Notices of the Royal Astronomical Society 2020-08-08

应用进化策略和微分修正法建立了一套多约束、多目标条件下的月球软着陆轨道设计方法. 根据中国发射场和火箭运载的实际情况, 给出了软着陆轨道需要满足的过程约束及终端条件, 提出了利用进化策略进行轨道初步设计,通过微分修正法对初步设计结果进行修正的软着陆轨道设计思路, 并采用STK进行了仿真和结果验算. 分析表明, 基于进化策略的初步设计能够为微分修正提供良好的初值, 保证了其收敛性. STK仿真结果验证了设计思路的有效性及结果的正确性. 本文提出的方法能够为月球软着陆轨道设计提供参考.

10.11728/cjss2012.01.092 article EN cc-by Chinese Journal of Space Science 2012-01-01

As a general model of unmanned systems, cyber physical system (CPS) usually faces variety interference from the domain and information domain. Resilience is key capability to ensure that CPS can still maintain its core business capabilities in face complex interference. This paper mainly analyzes research progress resilience. First, based on literature, statistical analysis resilience recent years conducted by using systematic mapping method. Then, three aspects resilience, namely, modeling,...

10.1109/icus55513.2022.9986856 article EN 2021 IEEE International Conference on Unmanned Systems (ICUS) 2022-10-28
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