Development and Flight Test of an Advanced Hydrofluidic Stabilization System
Final rept. 23 Nov 1971-10 Jun 1975
HONEYWELL INC MINNEAPOLIS MN GOVERNMENT AND AERONAUTICAL PRODUCTS DIV
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The objective of this program is to demonstrate the performance of an advanced hydrofluidic stabilization system that is designed to provide pilot relief modes within a highly reliable, low-cost system. The system was designed, built, and tested to obtain the desired performance, and then subjected to flightworthiness testing to ensure structural integrity. The system was then installed, flight tested, and evaluated in a UH-1M helicopter. The flight test results are discussed.
- Fluidics and Fluerics