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Title Details:
Stability Augmentation Systems and Auto-Pilots
Authors: Antoniadis, Ioannis
Reviewer: Vosniakos, Georgios-christoforos
Subject: ENGINEERING AND TECHNOLOGY > TECHNOLOGICAL SCIENCES AND ENGINEERING > AIRCRAFT TECHNOLOGY AND ENGINEERING > STABILITY AND CONTROL
ENGINEERING AND TECHNOLOGY > TECHNOLOGICAL SCIENCES AND ENGINEERING > AIRCRAFT TECHNOLOGY AND ENGINEERING
Description:
Abstract:
Pseudostatic stability derivatives. Calculation of stability derivatives. Longitudinal aerodynamic stability derivatives. Derivatives of the force due to velocity disturbance. Derivatives of the moment due to velocity disturbance. Derivatives of the moment due to pitching velocity disturbance. Derivatives due to acceleration disturbance. Lateral aerodynamic stability derivatives. Derivatives due to sideslip. Derivatives due to yaw rate. Derivatives due to roll rate. Stability derivatives of aerodynamic control. Derivatives due to elevator up-down.
Technical Editors: Paradeisiotis, Andreas
Type: Chapter
Creation Date: 2015
Item Details:
License: http://creativecommons.org/licenses/by-nc-nd/3.0/gr
Handle http://hdl.handle.net/11419/1761
Bibliographic Reference: Antoniadis, I. (2015). Stability Augmentation Systems and Auto-Pilots [Chapter]. In Antoniadis, I. 2015. Flight Dynamics and Control [Undergraduate textbook]. Kallipos, Open Academic Editions. https://hdl.handle.net/11419/1761
Language: Greek
Consists of: 1. Τόπος ριζών συστήματος διατήρησης του ύψους
2. Γεωμετρία τήρησης του ίχνους καθόδου
3. Σύστημα διατήρησης του ύψους (Full state feedback)
Is Part of: Flight Dynamics and Control
Publication Origin: Kallipos, Open Academic Editions