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Chapter 4

Chapter 4 Dynamical Equations for FlightVehiclesThese notes provide a systematic background of the derivation of the equations of motionfor a flight vehicle, and their linearization. The relationship between dimensional stabilityderivatives and dimensionless aerodynamic coefficients is presented, and the principalcontributions to all important stability derivatives for flight vehicles having left/rightsymmetry are Basic Equations of MotionThe equations of motion for a flight vehicle usually are written in a body-fixed coordinate is convenient to choose the vehicle center of mass as the origin for this system, and the orientationof the (right-handed) system of coordinate axes is chosen byconvention so that, as illustrated inFig.

• the z-axis lies in the symmetry plane of the vehicle, is perpendicular to the x-axis, and points ... New York to London, we certainly are interested in the heading, but this is not really an issue as far as analysis of the stability and controllability of the vehicle are concerned.

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Transcription of Chapter 4

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