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 store data from multiple sensors at multiple rates during launch, ascent, deployment and descent phases of the subsonic parachute test.
FPGA development for high altitude subsonic parachute testing
Military and Aerospace Programmable Logic Device International Conference ; 2005 ; Washington, DC, United States
2005-09-01
Conference paper
No indication
English
High altitude test program for a Mars subsonic parachute
NTRS | 2005
|High Altitude Test Program for a Mars Subsonic Parachute
AIAA | 2005
|