NTL Record

Title Simulation Model for the Piper PA-30 Light Maneuverable Aircraft in the Final Approach
Record ID 50374
Personal Name
Creator
Koziol, Joseph S., Jr.
Source 21p. in various pagings
Corporate Creator John A. Volpe National Transportation Systems Center (U.S.)
Corporate
Contributor
United States. Department of Transportation. Federal Aviation Administration
Publisher United States. Department of Transportation. Federal Aviation Administration
Publication Date 19710701
Language English
Abstract The report describes the Piper PA-30 'Twin Comanche' aircraft and a representative autopilot during the final approach configuration for simulation purposes. The aircraft is modeled by linearized six-degree-of-freedom perturbation equations referenced to the aircraft stability axis. Other equations are presented which derive the body axis rates, velocities and accelerations, and ground referenced velocities (translation equations). The autopilot is a representative system for automatic ILS approaches from initial localizer track down to decision height. The glideslope system is engaged by approaching the glidepath at constant altitude (usually in the altitud hold mode) on the localizer beam. The pilot must take over manually at the decision height since light aircraft are not normally equipped with automatic flare capability. The aircraft autopilot model described herein has been used extensively in simulation studies at TSC and exhibits the expected behavior.
Rosap ID dot:11762
Rosap URL https://rosap.ntl.bts.gov/view/dot/11762
TRT Terms Simulation; Automatic pilot (Ships); Aircraft; Approach; Instrument landing systems
Classification NTL - AVIATION - AVIATION;
NTL - AVIATION - Aviation Human Factors;
NTL - AVIATION - Aviation Safety/Airworthiness
Geographical
Coverage
United States
Report Number DOT-TSC-FAA-71-11
Resource type Research Paper
URL https://ntlrepository.blob.core.windows.net/lib/50000/50300/50374/733757.pdf
Format PDF
Database NTL Digital Repository