Launcher reusability is the most effective way of reducing access to space costs, but remains a great technical challenge for the European aerospace industry. One of the challenges lies in the recovery GNC strategy and algorithms, in particular those of the powered-landing phase, which must enable a precise landing with low fuel margins and significant dispersions. While state-of-the-art solutions for Navigation and control problems can be applied, namely, hybrid Navigation techniques and robust control, for the powered descent guidance problem novel techniques are required to enable on-board optimization, that is necessary to achieve the landing accuracy required to recover the first stage of a launcher. This paper presents the GNC solutio...
The next generation of reusable launch vehicles (RLVs) require significant improvements in guidance...
This thesis presents a guidance scheme for the Terminal Area Energy Management (TAEM) and Approach a...
This paper introduces a Reusable Launch Vehicle (RLV) descent dynamics simulator coupled with closed...
This paper presents the GNC concept solution developed for the recovery and landing of Vertical Take...
This paper presents the RETALT recovery mission GNC, with a focus on the GNC solutions for the power...
This paper presents the Guidance, Navigation and Control solution currently in development by DEIMOS...
The capability to partially recover and reuse a launch vehicle is currently the most effective way o...
In the frame of technology development for reusable launch vehicles and future planetary landing mis...
In recent years, reusability has become a dominant feature in the design of novel small launch vehic...
Abstract: The goal of this paper is to provide a critical review of different guidance, navigation a...
This work aims to demonstrate the benefits and limitations of an on-board Guidance for reusable laun...
The ESA REVLANSYS study aims to develop key technologies in the field of Mission Engineering and GNC...
Future launch vehicle concepts and technologies for expendable and reusable launch vehicles are curr...
In the last decade, the number of space-based applications increased dramatically. To cover such a d...
International audienceIn the context of the development of future launchers, Toss Back concepts are ...
The next generation of reusable launch vehicles (RLVs) require significant improvements in guidance...
This thesis presents a guidance scheme for the Terminal Area Energy Management (TAEM) and Approach a...
This paper introduces a Reusable Launch Vehicle (RLV) descent dynamics simulator coupled with closed...
This paper presents the GNC concept solution developed for the recovery and landing of Vertical Take...
This paper presents the RETALT recovery mission GNC, with a focus on the GNC solutions for the power...
This paper presents the Guidance, Navigation and Control solution currently in development by DEIMOS...
The capability to partially recover and reuse a launch vehicle is currently the most effective way o...
In the frame of technology development for reusable launch vehicles and future planetary landing mis...
In recent years, reusability has become a dominant feature in the design of novel small launch vehic...
Abstract: The goal of this paper is to provide a critical review of different guidance, navigation a...
This work aims to demonstrate the benefits and limitations of an on-board Guidance for reusable laun...
The ESA REVLANSYS study aims to develop key technologies in the field of Mission Engineering and GNC...
Future launch vehicle concepts and technologies for expendable and reusable launch vehicles are curr...
In the last decade, the number of space-based applications increased dramatically. To cover such a d...
International audienceIn the context of the development of future launchers, Toss Back concepts are ...
The next generation of reusable launch vehicles (RLVs) require significant improvements in guidance...
This thesis presents a guidance scheme for the Terminal Area Energy Management (TAEM) and Approach a...
This paper introduces a Reusable Launch Vehicle (RLV) descent dynamics simulator coupled with closed...