Introduction to Aircraft Flight Dynamics

丛 书 名：AIAA Education Series

作     者：Louis V. Schmidt 

I S B N：(纸本) 9781563472268 

出 版 社：American Institute of Aeronautics and Astronautics  Inc. 

出 版 年：1998年

页      数：410页

主 题 词：Aerodynamic Performance Aerodynamics Aeronautical Engineering Aeronautics Aerospace Manufacturers Aerospace Sciences Air Forces Aircraft Components and Structure Aircraft Control Aircraft Design Aircraft Dynamic Modes Aircraft Flight Control System Aircraft Instruments Aircraft Operations Aircraft Operations and Technology Aircraft Performance Aircraft Stability and Control Aircraft Wing Components Aircraft Wing Design Aircrafts Aircrew Airfoil Airfoil Nomenclature Airspeed Aviation Aviation Safety Aviation Weather Hazards Avionics Computers Civil Aviation Combat Aircraft Commercial Aviation Computational Fluid Dynamics Computer Programming and Language Computing and Informatics Computing, Information, and Communication Control Theory Finite Element Method Fixed-Wing Aircraft Flight Control Surfaces Flight Dynamics Flight Test Flight Training Flow Regimes Fluid Dynamics Fluid Flow Properties Flying Qualities Guidance, Navigation, and Control Systems Jet Aircraft Longitudinal Static Stability Military Aircraft Military Aviation Operating Systems Rotorcrafts Signal Processing Slip (Aerodynamics) Society and Aerospace Technology Software Systems Stability Augmentation Systems Systems Software Turbulence Turbulence Models Unsteady Aerodynamics Vortex Dynamics Wind Tunnels Wing Configurations Wing Planforms 

学科分类：080103[工学-流体力学] 08[工学] 080104[工学-工程力学] 082701[工学-核能科学与工程] 0827[工学-核科学与技术] 0801[工学-力学（可授工学、理学学位）] 

摘      要：Introduction to Aircraft Flight Dynamics is geared directly toward senior undergraduate engineering students and beginning graduate students. The author uses linear algebraic principles and notations to establish airframe equations of motion. The use of this dimensional approach to stability derivatives when describing aerodynamic forces and moments in the six governing relations assures that the solutions to given problems remain in real time and frequency. In addition, the textbook uses modern control theory concepts to introduce the airframe as a plant matrix operator. Consistent reference is made to matrix algebra-oriented software, MATLAB®, as a tool for solving aircraft-related problems in both the linear and nonlinear forms. Contemporary analytical methods are also employed to describe the aerodynamics involved in flight vehicle motion and to develop a rationale for modeling and solving related problems in aircraft dynamics. The author also discusses modern control theory methods.