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Performance, Static and Dynamic Stability, Classical Feedback Control, with State-Space and Rotorcraft Foundations
出版American Institute of Aeronautics and Astronautics, Incorporated, 2025
主題Technology & Engineering / Aeronautics & AstronauticsTransportation / General
ISBN16241072499781624107245
URLhttp://books.google.com.hk/books?id=QaoM0QEACAAJ&hl=&source=gbs_api
註釋"Introduction to Aircraft Flight Mechanics, Third Edition revises and expands this acclaimed, widely adopted textbook. Outstanding for use in undergraduate aeronautical engineering curricula, it is written for those first encountering the topic by clearly explaining the concepts and derivations of equations involved in aircraft flight mechanics. It begins with a review of basic aerodynamics and propulsion and continues through aircraft performance, equations of motion, static stability, linearizing equations of motion, dynamic stability, classical feedback control, stability and control augmentation, Bode, state space, and special topics. The third edition includes extensive updates to the first ten chapters and new chapters covering propeller theory and rotocraft analysis. Chapter 13 provides interesting design insights on the A-10 Close Air Support aircraft"--