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Extends dynamics to trajectory propagation over an Earth model with coordinate transformations, derives state variables, and presents airframe, engine, and standard atmosphere modeling plus numerical integration techniques. 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Konyak  \nPrepared for:  \nScott Doucett  \nANG-E161  \nSimulation Branch, Laboratory Services Division  \nFederal Aviation Administration  \nWilliam J. Hughes Technical Center  \nAtlantic City, NJ 08405  \nUnder:  \nAir Traffic Engineering Co., LLC  \n1027 Route 9 South  \nPalermo, NJ 08223  \nFAA Prime Contract No. DTFAWA-10A-00020  \nOctober 2012  \nAcknowledgments  \nThis project was supported under contract No. DTFA03-94-C-0042 (CADSS) with the Federal Aviation Administration William J. Hughes Technical Center, Atlantic City, NJ, under subcontract to System Resources Corporation (SRC) . The author acknowledges the insightful project direction provided by Mr. Dan Warburton of the FAA and Mr. George Chachis of SRC, during the course of this work. The author also wishes to acknowledge the various technical contributions and reviews from the members of the Seagull team. Specifically, the author acknowledges Dr. John Sorensen and Tysen Mueller for their contributions to the error modeling sections of the Navigator development, and George Hunter and JC Gillmore for their leadership and guidance throughout the project.  \nMark Peters September, 1999  \nTHIS PAGE INTENTIONALLY LEFT BLANK  \nii  \nTable of Contents  \n1. INTRODUCTION....................................................................................................1  \n1.1 BACKGROUND .........................................................................................................1  \n1.2 SCOPE ......................................................................................................................2  \n1.3 ORGANIZATION .......................................................................................................2  \n2. THE AIRCRAFT EQUATIONS OF MOTION ...................................................5  \n2.1 THE DEFINITION OF THE BODY FRAME AND THE INERTIAL FRAME .........................5  \n2.2 DEFINITION OF FLIGHT MECHANICS NOMENCLATURE.............................................8  \n2.3 THE WIND AND STABILITY REFERENCE FRAMES .....................................................9  \n2.4 THE DERIVATION OF THE SIX DEGREE OF FREEDOM EQUATIONS OF MOTION .......12  \n2.5 THE MODAL PROPERTIES OF THE SIX DEGREE OF FREEDOM MODEL .....................16  \n2.5.1 The Short Period Mode .................................................................................. 18  \n2.5.2 The Phugoid Mode ......................................................................................... 18  \n2.5.3 The Dutch Roll Mode ..................................................................................... 18  \n2.5.4 The Roll Mode ................................................................................................ 19  \n2.5.5 The Spiral Mode ............................................................................................. 19  \n2.6 SIMPLIFYING THE EQUATIONS OF MOTION TO FOUR DEGREES OF FREEDOM .........20  \n2.7 THE ADDITION OF WINDS ......................................................................................27  \n2.8 TRAJECTORY PROPAGATION OVER AN EARTH MODEL ..........................................31  \n2.8.1 Elliptic Earth Reference Frames ................................................................... 31  \n2.8.2 The Earth Model and its Kinematic Parameters ........................................... 35  \n2.8.3 Kinematics Relating the Coordinate Frames................................................. 39  \n2.8.4 Transforming DIS to Lat/Lon ........................................................................ 43  \n2.9 THE DERIVED STATE VARIABLES ..........................................................................45  \n2.10 THE AIRFRAME MODEL......................................................................................47  \n2.11 THE ENGINE MODEL ..........................................","cbCaid1JgAcQ1HnT","https://ap.wps.com/l/cbCaid1JgAcQ1HnT","pdf",4491568,321,"English","# INTRODUCTION\n## BACKGROUND\n## SCOPE\n## ORGANIZATION\n# THE AIRCRAFT EQUATIONS OF MOTION\n## THE DEFINITION OF THE BODY FRAME AND THE INERTIAL FRAME\n## DEFINITION OF FLIGHT MECHANICS NOMENCLATURE\n## THE WIND AND STABILITY REFERENCE FRAMES\n## THE DERIVATION OF THE SIX DEGREE OF FREEDOM EQUATIONS OF MOTION\n## THE MODAL PROPERTIES OF THE SIX DEGREE OF FREEDOM MODEL\n## SIMPLIFYING THE EQUATIONS OF MOTION TO FOUR DEGREES OF FREEDOM\n## THE ADDITION OF WINDS\n## TRAJECTORY PROPAGATION OVER AN EARTH MODEL\n## THE DERIVED STATE VARIABLES\n## THE AIRFRAME MODEL\n## THE ENGINE MODEL\n## THE STANDARD ATMOSPHERE MODEL\n## INTEGRATION TECHNIQUES\n## THE INTEGRATION OF THE ROLL EQUATION\n## DESIGN OF THE LATERAL CONTROL SYSTEM\n# THE EXAMINATION OF THE LONGITUDINAL DYNAMICS\n## THE LINEAR MODEL OF THE LONGITUDINAL DYNAMICS\n## THE ANALYSIS OF LONGITUDINAL AIRCRAFT MODAL PROPERTIES\n## TRANSFER FUNCTION ANALYSIS OF THE LONGITUDINAL DYNAMICS\n# THE FEEDBACK CONTROL SYSTEM FOR LONGITUDINAL CONTROL","[{\"question\":\"What is the purpose of the aircraft dynamics model in this report?\",\"answer\":\"It provides an engineering analysis and design of an aircraft dynamics model specifically for the FAA Target Generation Facility.\"},{\"question\":\"How does the report structure the aircraft motion modeling?\",\"answer\":\"It derives six degrees of freedom equations of motion, analyzes modal properties, then simplifies the model to four degrees of freedom and adds wind effects.\"},{\"question\":\"What numerical and system components are included for simulation?\",\"answer\":\"The report includes airframe and engine models, a standard atmosphere model, numerical integration techniques, and the integration of roll dynamics.\"}]","The Engineering Analysis and Design of the Aircraft Dynamics Model for the FAA Target Generation Facility - Prepared Report | PDF",1792850504,809]