Maximilian Roth

Title: "Non linear optimal control strategies for geostationary spacecraft orbit station keeping using electric propulsion only" The main objective of this thesis is indeed to develop optimal control strategies in order to keep a geostationary spacecraft within its allocated control box using electric propulsion only.

Title: "Control design, automatic optimisation and verfication for a fin acctuator"

- Design and simulation of VHDL code in Lattice Diamond incl. functional testing - Documentation of the designed system and of the tests - Design of SPI, SSI and I2C interfaces - Development of logic for BLDC motors and memory management for a FPGA

Control Systems for Spacecrafts and Aircrafts, Optimal Control, Space Systems

Space Physics, Spacecraft Environment Interactions, Electronics in Space, Optics and Radar based Observations

Space physics, Spacecraft System Design, Space Dynamics, Internet Technologies

Aerospace, computer science, embedded systems, flight dynamics, control, optimal control, physics, FGPA