Fabrication And Design Integration of an Electronic Control Unit for a Dual Mode Electro/Pneumatic Actuator for the T-2C Aircraft
Abstract
Report of the design, fabrication and test of Electronic Control Unit (ECU) for Dual Mode Electro/Pneumatic Actuator. Integration tests establish control capability of ECU in both pneumatic and electric modes. Closed-loop operation fully implemented in design. Evaluation restricted to open-loop due to limited actuator performance.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1981
- Accession Number
- ADA358746
Entities
People
- James Himich
- Wallace Kineyko