Title :
Model-based GN&C simulation and flight software development for Orion missions beyond LEO
Author :
Odegard, Ryan ; Milenkovic, Zoran ; Henry, Joseph ; Buttacoli, Michael
Author_Institution :
Draper Lab., Houston, TX, USA
Abstract :
For Orion missions beyond low Earth orbit (LEO), the Guidance, Navigation, and Control (GN&C) system is being developed using a model-based approach for simulation and flight software. Lessons learned from the development of GN&C algorithms and flight software for the Orion Exploration Flight Test One (EFT-1) vehicle have been applied to the development of further capabilities for Orion GN&C beyond EFT-1. Continuing the use of a Model-Based Development (MBD) approach with the Matlab®/Simulink® tool suite, the process for GN&C development and analysis has been largely improved. Furthermore, a model-based simulation environment in Simulink greatly eases the process for early, rapid development of flight algorithms. The benefits seen by employing lessons learned from EFT-1 are described, as well as the approach for implementing additional MBD techniques. Also detailed are the key enablers for improvements to the MBD process, including enhanced configuration management techniques for model-based software systems, automated code and artifact generation, and automated testing and integration.
Keywords :
aerospace control; aerospace simulation; aerospace testing; aircraft navigation; celestial mechanics; control engineering computing; EFT-I vehicle; LEO; MBD approach; Matlab-Simulink tool suite; Orion mission; artifact generation; automated code; automated testing; enhanced configuration management techniques; exploration flight test one vehicle; flight software development; guidance navigation and control system; low Earth orbit; model-based GN&C simulation; model-based development approach; Biological system modeling; Extraterrestrial measurements; MATLAB; Mathematical model; NASA; Navigation;
Conference_Titel :
Aerospace Conference, 2014 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5582-4
DOI :
10.1109/AERO.2014.6836230