Integrated Pilot Assist System.
Abstract
This program was originated for the purpose of developing a flight control system for helicopters and V/STOL vehicles. The design utilizes force stick steering and parallel servo installation with full, mechanical back-up. The system stabilizes the vehicle in all four axes with additional features such as altitude hold velocity hold, turn coordination, and attitude hold. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1973
- Accession Number
- AD0913469
Entities
People
- Arthur J. Welch
- William L. Young Jr.
Organizations
- Flight Dynamics Laboratory