A STUDY OF AN AUTOMATIC POWER COMPENSATOR WITH AIRSPEED AND ANGLE OF ATTACK AS CONTROLLING INPUTS.
Abstract
A study of an Automatic Power Compensator with inputs of airspeed and angle of attack was conducted by means of a simplified analytical analysis and analogue simulation. Digital Computer programming was used for data reduction. The F-8 aircraft was used as the vehicle for the study. Loop gains were initially set by means of a simplified analysis on the indepent phugoid and short period motions. The validity of such an analysis was demonstrated by analogue simulation of the complete system. The system is feasible both for independent use or as a component of a complete automatic flight system.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1966
- Accession Number
- AD0486366
Entities
People
- Richard Appleton Mcconnel
Organizations
- Naval Postgraduate School