Publication Date:
2019-07-13
Description:
In this paper we will give a brief overview of how different missions implemented the fault protection application and the improvements along the way. We will then propose an architecture that supports the direct implementation of state-chart models into flight code. These state-chart models can be used to formally and naturally specify the behavior of all the major fault protection components - monitors, fault protection engine, and fault responses. The goal is a flexible, light-weight implementation of a traditional fault protection software system that is inexpensive to implement, reliable and understandable for both system and software developers.
Keywords:
Computer Programming and Software
Type:
AIAA Infotech @ Aerospace Meeting; Apr 07, 2009 - Apr 09, 2009; Seattle, WA; United States
Format:
text