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Advanced flight dynamics with elements of flight control / Nandan K. Sinha and N. Ananthkrishnan

By: Contributor(s): Resource type: Ressourcentyp: Buch (Online)Book (Online)Language: English Publisher: Boca Raton ; London ; New York : CRC Press, [2017]Copyright date: © 2017Description: 1 Online-Ressource (xviii, 348 pages)ISBN:
  • 9781315151977
  • 9781498746069
Subject(s): Additional physical formats: 9781498746045. | 9781138746039. | Erscheint auch als: Advanced flight dynamics with elements of flight control. Druck-Ausgabe Boca Raton : CRC Press, Taylor & Francis Group, 2017. xviii, 348 SeitenDDC classification:
  • 629.132/3
RVK: RVK: ZO 7230 | ZO 7250LOC classification:
  • TL570
Online resources: Summary: 1.8.2 Propulsive Moment1.9 Selection of Equations for Specific Problems; 1.9.1 Simulation of Arbitrary Maneuver; 1.9.2 Steady States Such as Level Flight, Shallow Climb/Descent, Horizontal Turn, Spin, Etc.; 1.9.3 Longitudinal Flight Steady States; 1.9.4 Constant-Velocity Flight in the Longitudinal Plane; 1.9.5 Constant-Velocity Rolling Maneuvers; 1.10 Equations of Motion in the Presence of Wind; Reference; Chapter 2: Modeling and Interpreting the Aerodynamics; 2.1 Definition of Aerodynamic Coefficients; 2.2 Modeling of Aerodynamic Coefficients; 2.3 Static Aerodynamic Coefficient TermsSummary: 2.3.1 Longitudinal Coefficients with Angle of Attack2.3.2 Lateral Coefficients with Angle of Attack and Sideslip Angle; 2.3.3 Variation with Mach Number; 2.3.4 Variation with Control Surface Deflection; 2.4 Dynamic Aerodynamic Coefficient Terms; 2.4.1 Pitching Moment Due to Relative Pitch Rate,Cmq1; 2.4.2 Yawing and Rolling Moment Due to Relative Yaw Rate, Cnr1 and Clr1; 2.5 Flow Curvature Coefficient Terms; 2.5.1 Yawing and Rolling Moment Due to Wind-Axis Yaw Rate, Cnr2 and Clr2; 2.5.2 Pitching Moment Due to Wind-Axis Pitch Rate, Cmq2; 2.5.3 Rolling Moment Due to Wind-Axis Roll Rate, Clq2Summary: 2.6 Downwash Lag Terms2.7 Sample Simulation Cases; 2.7.1 Example Airplane and Aerodynamic Models; 2.7.1.1 F-18 Low-Angle-of-Attack Model; 2.7.1.2 F-18/HARV High-Angle-of-Attack Model; 2.7.1.3 Pseudo-Steady-State Model for Rapid Rolling Maneuvers; 2.7.2 Example Simulation Results; References; Chapter 3: Introduction to Dynamical Systems Theory; 3.1 Types of Steady States; 3.1.1 Equilibrium States; 3.1.2 Periodic States; 3.1.3 Quasi-Periodic States; 3.1.4 Chaotic States; 3.2 Stability of Steady States; 3.2.1 Stability of Equilibrium States; 3.2.2 Stability of Periodic OrbitsSummary: Cover; Half Title; Title Page; Copyright Page; Contents; Preface; Authors; Chapter 1: Six Degrees of Freedom Equations of Motion; 1.1 Definition of Axis Systems; 1.1.1 Body-Fixed Axis System; 1.1.2 Earth-Fixed Axis System; 1.1.3 Wind-Fixed Axis System; 1.2 Definition of Variables; 1.3 3-2-1 Transformation; 1.3.1 Earth- and Body-Fixed Axes; 1.3.2 Earth- and Wind-Fixed Axes; 1.3.3 Wind- and Body-Fixed Axes; 1.3.4 Relation between the Body-Axis and Wind-Axis Euler Angles; 1.4 Relation between Angular Velocity Vector and Euler Angle RatesPPN: PPN: 1039989918Package identifier: Produktsigel: ZDB-4-NLEBK
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