Real-Time Flight Engine Controller Using NI LabVIEW and CompactRIO Hardware
Abstract
The Challenge: Designing a light-weight, low-cost control and data system for the engine controller and a remote data system for propellant conditioning for an Air Force SBIR Phase III vortex propulsion flight demonstration program. The Solution: Developing a low cost, off-the-shelf embedded system with minimal manpower and increased flexibility using a custom NI LabVIEW application and the NI CompactRIO platform to deterministically control a liquid rocket engine and its associated feed systems. Additionally developing an easy to setup remote temperature monitoring system.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 15, 2011
- Accession Number
- ADA546033
Entities
People
- Joan Hoopes