Effect of Gun Pulse on Helicopter Attitudes.
Abstract
Computer programs have been devised to calculate both steady state pitch attitude and dynamic pitch response to a pulse, gun-initiated moment of a typical helicopter. It is shown that for large fixed gun pulses the resulting motions may be difficult to control. A critical condition is the ability to hold position and attitude at hover.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1976
- Accession Number
- ADA023461
Entities
People
- R. R. Oehrli
Organizations
- United States Army Materiel Systems Analysis Activity