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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2010, Vol. 31 ›› Issue (9): 1841-1848.

• Avionics and Autocontrol • Previous Articles     Next Articles

Real-time Attitude Planning for Low RCS Micro-satellites with Limited Attitude Control Ability

Su Kang, Zhou Jianjiang   

  1. College of Information Science and Technology, Nanjing University of Aeronautics and Astronautics
  • Received:2009-09-28 Revised:2010-03-12 Online:2010-09-25 Published:2010-09-25
  • Contact: Zhou Jianjiang

Abstract: A real-time satellite attitude planning algorithm (RSAPA) is developed for low radar cross section (RCS) micro-satellites with limited attitude control energy and abilities to enhance their on-orbit operational effectiveness and survivability. Based on the curved surface pixel method (CSPM), finite difference time domain (FDTD) and hypothesis testing, novel micro-satellite RCS and radar detection probability mathematical models are established in a three-dimensional (3D) space, and the relative radar threat evaluation function and planning cost evaluation function are defined according to a novel radar distribution model. Particle swarm optimization (PSO) algorithm is applied to the planning to decrease the algorithm computational complexity and improve its real-time performance. In the simulation, within limited computational complexity and planning cost, the algorithm reduces effectively the micro-satellite’s RCS and radar detection probability in threat directions, and meets the needs of real-time micro-satellite attitude planning.

Key words: attitude planning, micro-satellite, radar cross section, particle swarm optimization, computational complexity

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