Description
Dynamics, control, and flying qualties of v/stol aircraft
Author: FRANKLIN James
Language: EnglishApproximative price 101.82 €
Subject to availability at the publisher.
Add to cart the book of FRANKLIN James
Publication date: 07-2002
300 p. · 19.8x12.6 cm · Hardback
300 p. · 19.8x12.6 cm · Hardback
Description
/li>Contents
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This text presents the principles of dynamics and control for vertical, short take-off landing (V/STOL) aircraft. It is the first book of its kind.
The book is intended for graduate students and professionals in aeronautics who have knowledge of linear systems analysis, aircraft static and dynamic stability and control.
The text begins with a discussion of V/STOL aircraft operations. Control strategies, equations of motion, longitudinal and lateral-directional flying qualities in both hover and forward flight, wind and turbulence responses, and control augmentation and cockpit displays are covered. Specific examples of the YAV-8B Harrier and XV-15 Tilt Rotor aircraft are used to illustrate actual V/STOL dynamic and control characteristics.
The book is intended for graduate students and professionals in aeronautics who have knowledge of linear systems analysis, aircraft static and dynamic stability and control.
The text begins with a discussion of V/STOL aircraft operations. Control strategies, equations of motion, longitudinal and lateral-directional flying qualities in both hover and forward flight, wind and turbulence responses, and control augmentation and cockpit displays are covered. Specific examples of the YAV-8B Harrier and XV-15 Tilt Rotor aircraft are used to illustrate actual V/STOL dynamic and control characteristics.
- Introduction
- Representative Operations of V/STOL Aircraft
- Control Strategy and Desired Control Characteristics
- Equations of Motion for Hover and Forward Flight
- Longitudinal Flying Qualities in Hover
- Lateral-Directional Flying Qualities in Hover
- Longitudinal Flying Qualities in Forward Flight
- Lateral-Directional Flying Qualities in Forward Flight
- Response to Wind and Turbulence
- Control Augmentation and Cockpit Displays
- Appendices
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