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Springer Aerospace Stability and Control Vehicle Design Book

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Description

This Springer Aerospace Technology publication presents the AeroMech methodology for the stability and control of both conventional and unconventional aerospace vehicle configurations. The text provides a generic approach suitable for designs ranging from subsonic to hypersonic speeds. By utilizing non-linear vortex lattice aerodynamics combined with static and dynamic equations of motion, the book enables the sizing of primary control effectors for fixed wing aircraft. It addresses the complex task of harmonizing control power demands with requirements for static, dynamic, and maneuver stability. Furthermore, the analysis accounts for the six-degree-of-freedom trim state, offering a comprehensive technical resource for engineers working across various flight regimes.

Key Features

Introduces the AeroMech methodology for sizing primary control effectors in fixed wing designs.

Covers a wide range of flight regimes from subsonic to hypersonic speeds.

Provides analysis for both conventional and unconventional aerospace vehicle configurations.

Integrates non-linear vortex lattice aerodynamics with static and dynamic equations of motion.

Balances control power demands with static, dynamic, and maneuver stability requirements.

Includes considerations for the six-degree-of-freedom trim state in stability analysis.

Product Specifications

Format
paperback
Domain
Amazon UK
Release Date
14 August 2020
Listed Since
08 August 2020

Barcode

No barcode data available

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