This document deals with an algorithm for generating Ideal Handling Quality Models for the Longitudinal Axes of modern high performance aircraft when a flight condition is specified. The technique solves a set of non-linear equations which express the performance requirements in terms of the unknown equivalent aircraft stability and control derivatives of the ideal models. The software package is developed using PC-MATLAB and the ideal HQ models are analyzed using the HQ package already developed. The designer can directly incorporate the ideal HQ models as reference models for his feedback synthesis.
Ideal Aircraft Handling Quality Models: Longitudinal Axis
1992
18 pages
Report
No indication
English
Analysis of aircraft longitudinal handling qualities
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