One of the future flagship missions of the European Space Agency is the asteroid sample return mission Marco-Polo. Although there have been a number of past missions to asteroids, a sample has never been successfully returned. The return of asteroid regolith to the Earth's surface introduces new technical challenges. This article develops attitude control algorithms for the descent phase onto an asteroid in micro-gravity conditions and draws a comparison between the algorithms considered. Two studies are also performed regarding the fault detection isolation and recovery of the control laws considered. The potential of using direct adaptive control (DAC) as a controller for the surface sampling process is also investigated. The use of a DAC...
The advancement of asteroidal surface science necessitates in-situ science collection by robotic lan...
The exploration of deep space presents a variety of significant control challenges. Long communicati...
This paper considers an optimal guidance law for the initial braking phase of a soft landing mission...
One of the future flagship missions of the European Space Agency is the asteroid sample return missi...
One of the future flagship missions of the European Space Agency (ESA) is the asteroid sample return...
Exploration of small planetary bodies is a fast growing field of interest. Compared to the explorat...
Spacecraft dynamics and control in the vicinity of an asteroid is a challenging and exciting problem...
Within this thesis, methods for on-board trajectory optimization and optimal control regarding diffe...
The Asteroid Impact and Deflection Assessment (AIDA), is an upcoming mission resulting from the coll...
NASA's Asteroid Redirect Robotic Mission (ARRM) aims to pick up a boulder from of a large asteroid a...
Future NASA missions include in-situ scientific explorations of small interplanetary objects like co...
Asteroid missions are gaining interest from the scientific community and many new missions are plann...
Near Earth Asteroids could potentially cause a great deal of devastation if one were to impact the E...
Near Earth Asteroids could potentially cause a great deal of devastation if one were to impact the E...
Autonomous GNC systems are one of the enabling technologies for many of the future ESA exploration ...
The advancement of asteroidal surface science necessitates in-situ science collection by robotic lan...
The exploration of deep space presents a variety of significant control challenges. Long communicati...
This paper considers an optimal guidance law for the initial braking phase of a soft landing mission...
One of the future flagship missions of the European Space Agency is the asteroid sample return missi...
One of the future flagship missions of the European Space Agency (ESA) is the asteroid sample return...
Exploration of small planetary bodies is a fast growing field of interest. Compared to the explorat...
Spacecraft dynamics and control in the vicinity of an asteroid is a challenging and exciting problem...
Within this thesis, methods for on-board trajectory optimization and optimal control regarding diffe...
The Asteroid Impact and Deflection Assessment (AIDA), is an upcoming mission resulting from the coll...
NASA's Asteroid Redirect Robotic Mission (ARRM) aims to pick up a boulder from of a large asteroid a...
Future NASA missions include in-situ scientific explorations of small interplanetary objects like co...
Asteroid missions are gaining interest from the scientific community and many new missions are plann...
Near Earth Asteroids could potentially cause a great deal of devastation if one were to impact the E...
Near Earth Asteroids could potentially cause a great deal of devastation if one were to impact the E...
Autonomous GNC systems are one of the enabling technologies for many of the future ESA exploration ...
The advancement of asteroidal surface science necessitates in-situ science collection by robotic lan...
The exploration of deep space presents a variety of significant control challenges. Long communicati...
This paper considers an optimal guidance law for the initial braking phase of a soft landing mission...