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Guidance development for winged and capsule reentry vehicles, e.g. Hopper, CapRee and X38, enabling high precision landing while considering all applicable constraints.


Control systems design of dynamic systems:
  • Attitude and orbit control of space- and aircrafts, which are assumed to be inelastic.
  • Control system design using multi-disciplinary modelling, e.g. for aeroelastic controllers, which consider the correlation between structure-mechanical distorsion and stationary and instationary aerodynamic forces and moments.
  • Autonomous aircraft control.

Safety Analyses

Comprehensive support for vehicle and mission safety assessments:

Class 3 Amateur Rockets FAA Waiver Application

Computation of the required data to fill in the Federal Aviation Administration application waiver for a Class 3 rocket. Read more...