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By Jan Roskam

ISBN-10: 1884885179

ISBN-13: 9781884885174

ISBN-10: 1884885187

ISBN-13: 9781884885181

Moment Library replica. San Diego Air and area Museum.

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Extra resources for Airplane Flight Dynamics and Automatic Flight Controls

Sample text

Be showntQ be the drag. jet forces respectively. FT = iFT, + jFTY + kFT, (U8b) for the thrust force components. g= igx + jgy + kg z (U8c) for the CO'mJODents of a-rayitational acceleration. joa- moment. Wtchina- moment and yawina- mOment respes;tiyely. " (U8e) for the thrust moment components: rolling moment. pectiyely. \. Velocities: ii3 = iP + jQ + kR (U8f) for the aniUlar velocity components: roll rate. pitch rate and yaw rate respectively. jaear velocity compopents: forward velocity. side velocity and downward velocity reSllectiyely.

In either case, general solutions to the equations can be obtained only by numerical integration. However, from an airplane design and from a handling qualities viewpoint there are two special flight conditions for which solutions of these equations are of primary interest: 1. Steady state flight conditions 2. flight conditions The remainder of this text is primarily concerned with the smdy and applications of the ' general' airplane equations of motion to these two sets of flight conditions. • Definition 1: Steady State Flight • A steady state ffight condition is dermed as one for which ALL motion variables remain constant with time relative to the body-rlXed axis systeill XYZ.

76) to small perturbations only! ) this assumption is not very restrictive from a pragmatic viewpoint. Even fighter and attack ait{>lanes operate mostly under conditions where small perturbations are desired: ordnance delivery ~uracy partly depends on that! Exceptions to this behavior are when airplanes are intentionally maneuvered to the edge of their flight envelope and/or airplanes which are encountering gust upsets. 4S). 77c) Rl +r = ('PI . 4 are obtained. 57). 4 without loss of generality.

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Airplane Flight Dynamics and Automatic Flight Controls by Jan Roskam


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