Since the first CubeSat launch in 2003, the hardware and software complexity of the
nanosatellites was continuosly increasing. To keep up with the continuously increasing …

The introduction of more onboard autonomy in future single and multi-satellite missions is
both a question of limited onboard resources and of how far can we actually thrust the …

The purpose of this work is to unify the communication and software interfaces of
heterogeneous mission components, covering both low-power embedded systems and …

ADCS= attitude determination and control system DTN= delay tolerant networking ECC=
error correction code GBO= goal based operations GS= ground station GSN= ground station …

Nanosatellite design and operations is a constant struggle for resources, whether they be
volume, communications bandwidth, electrical or processing power. Operating a …

This paper presents a new concept for hardware-in-the-loop testing of formation flying
control of small satellites. Instead of commonly used mobile units based on air cushion …

One of the most important challenges involved in the formation flight of satellites is that of
state estimation in terms of relative and inertial estimates. In near earth spacecraft GPS …