This paper describes a rapid, top down requirements-driven design of an FPGA used in an Earth qualification test program for a new Mars subsonic parachute. The FPGA is used to process and control storage of telemetry data from multiple sensors throughout; launch, ascent, deployment and descent phases of the subsonic parachute test.
High altitude subsonic parachute field programmable gate array
Military and Aerospace Programmable Logic Device International Conference ; 2005 ; Washington, DC, United States
2005-06-01
Conference paper
No indication
English
High Altitude Test Program for a Mars Subsonic Parachute
AIAA | 2005
|High altitude test program for a Mars subsonic parachute
NTRS | 2005
|