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Navigation and Control Systems



A spacecraft’s orbit and position must be precisely and actively controlled. This is managed using a combination of sensors, actuators and onboard data processing. The Navigation and Control Systems department is concerned with research and development of future seminal and/or strategic relevant technologies in the following areas:
Attitude and Orbit Control Systems
attitude and orbit control systems

Technology

  • Development of guidance, navigation and control systems for space applications
  • Simulation of spacecraft orbit and position dynamics and control systems
  • System analysis of orbit and position control subsystems 
  • Test and verification of orbit and position control systems and components

Applications

  • Satellite formation flying
  • Integrated navigation systems for space applications
  • Terrain based navigation for exploration missions
  • Verification of navigation and control systems
  • Simulation of Orbit and Position Control Systems

Projects

  • SHEFEX-2 navigation experiment
  • SHEFEX III
  • AsteroidFinder
  • ATON

Test Facilities

  • TRON
  • TEAMS 
  • FACE
  • GPS/INS
  • HILT

Software

  • HPS

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