Technical Paper

Autopilot System Tuning

931605

10/1/1993

Event
SAE Brasil
Authors
Luiz C. Marengo EMBRAER
Takashi Yoneyama EMBRAER
Abstract
Content
A new computational method was developed that enables preliminary tuning of Auto Pilot System internal parameters based on time response analysis of the aircraft and its auto pilot. This method main purpose is to reduce flight tests during Auto Pilot calibration procedure.
Meta Tags
Topics
Flight control systems
Flight dynamics
Automatic pilots
Aerodynamics
Electronic control units
Control systems
Aircraft
Landing gear
Mathematical models
Systems engineering
Materials
Interiors, Cabins, and Cockpits
Chassis
Cruise control
Transportation Systems
Steel
Design Engineering and Styling
Electric vehicles
Fuel economy
Underride guards
Affiliated or Co-Author
EMBRAER
Details
Citation
Marengo, L. and Yoneyama, T., "Autopilot System Tuning," SAE Brasil, Sao Paulo, Brazil, May 1, 1993, https://doi.org/10.4271/931605.
Additional Details
Publisher
SAE International
Published
10/1/1993
Product Code
931605
Content Type
Technical Paper
Language
English