1993-10-01

Autopilot System Tuning 931605

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.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

NASA Heavy Lift Rotorcraft Systems Investigation

2005-01-3149

View Details

TECHNICAL PAPER

A Preliminary Evaluation Test of GPS/DGPS Navigation System

940012

View Details

TECHNICAL PAPER

A VSAERO Analysis of Several Canard Configured Aircraft - Part 2

892287

View Details

X