Thesis - Leigh Moody.pdf - Bad Request - Cranfield University

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Chapter 8 / Simulation _ _ field is re-selecting, the cursor is placed at the end of the text, and the delete key is used. There are 12 graph control buttons labelled GRA1 to GRA12 selected using the left-hand mouse button. These buttons invoke separate pop-up windows for each variable containing a revolving time base graph, automatically scaled and presented in display units; an example of which is shown in Figure 8-12. Figure 8-12 : Rolling Graphics Window A new point is drawn on the graph at the windows refresh rate. Each graph is scaled to display the maximum value of the input signal. If the current limit is exceeded the graph is re-scaled and a “↓“ symbol is displayed above the upper limit guide and the scale values increased by a factor of 2. When a GRA button is de-activated the graph automatically disappears and all limits are reset if re-activated. 8.7.3 Target Wire Frame Window Critical points associated with target designation and tracking are dipicted on a wire frame representation of the following targets: • Backfire ( I_BACKFIRE ) • F15 ( I_F15 ) • Flogger ( I_FLOGGER ) 8-24 • F106 ( I_F106 ) • Flanker ( I_FLANKER ) • Fulcrum ( I_FULCRUM ) The simulation modules shown in brackets above are used to initialise the selected wire frame target model. Embedding the initialisation modules in the target visualisation software allows the user to change the target type interactively. The facet co-ordinates are defined in data files with the extension “*.GEO”, taking the name listed above. The facets are drawn in order, starting with those whose range is greatest along the LOS. This hidden facet layering technique removes lines that would naturally be hidden from view, as shown in Figure 8-13. The range to the target from the origin of the viewing axis chosen is displayed at the bottom of the window together with the image processing state (unused). 8.7.3.1 Control Menu The CONTROL menu provides the usual RUN, STEP and STOP controls and a ZOOM facility. This toggles between a target viewed in perspective
Chapter 8 / Simulation _ _ with the red viewing circle expanded to the size of the window (as shown in Figure 8-13), and a view in which the target is enlarged to fill the window. 8.7.3.2 Aim Point Menu The AIMPOINTS menu provides a list of critical points that can be displayed, all turned off by default. Next to each aim-point is an indicator, the colour of which corresponds to the colour of the symbol displayed when selected using the left-hand mouse button. The key to these symbols and their colours is given in the Table 8-1. The first two symbols are the position of the viewing axis and the reference point of the target (t) at its range from the viewing axis origin. 8.7.3.3 Axis Button This AXIS button controls the target view. The left-hand mouse button is used to toggle between the viewing options thereby setting AXISVIEW. The target body is aligned with Target Velocity axes (target reference) and is presented with respect to the viewing axis at the target range. The user is provided with 5 aim-point sets that depend on AXISVIEW cycled by clicking on the AXIS button. Characterisation of the sets is listed in Table 8-2 to Table 8-6. The red circle is centred on the reference axis, and its diameter depends on the viewpoint: • Radar beam-width or target-missile differential angle, C 1 8-25 M ( ξ , ) R : = max ξ TBW T Equation 8.7-1 • Radar beam-width, combined IMM estate, and the individual IMM filter estimates of the angle between the Alignment and Target frames, C2 T T1 T2 T3 T4 ( ξ , ξˆ , ξˆ , ξˆ , ξˆ , ˆ ) R : = max ξ TBW IMM A A A A A Equation 8.7-2 • Seeker beam width, Missile Velocity, Seeker Head, and estimated Missile Body, Missile Velocity and Seeker angles, C3 MV H B MV S ( ξ , ξ , ξ , ξˆ , ξˆ , ˆ ) R : = max ξ SBW • Seeker beam width, Missile Velocity, Seeker Head, and equivalent estimated angles, C4 A A MV H MV S ( ξ , ξ , ξ , ξˆ , ˆ ) R : = max ξ SBW B B A B A B A Equation 8.7-3 Equation 8.7-4
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CRANFIELD UNIVERSITY LEIGH MOODY SE
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ABSTRACT When considering advances
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Contents _ _ LIST OF CONTENTS 1 INT
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Contents _ _ 8.2 The Scope of Moder
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Contents _ _ 17.4 Inertial Velocity
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Tables _ _ LIST OF TABLES Table 1-1
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Figures _ _ LIST OF FIGURES Figure
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Figures _ _ Figure 5-1 : Centralise
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Figures _ _ Figure 19-3 : Air Densi
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Acronyms _ _ Acronyms And Abbreviat
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Acronyms _ _ HDOP - NAVSTAR GPS Hor
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Acronyms _ _ RCS - Radar Cross Sect
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Glossary _ _ GLOSSARY A challenge w
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Glossary _ _ 0.1 Predicate Calculus
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Glossary _ _ ]A,B] Real number rang
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Glossary _ _ 0.9 Matrix Operators [
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Glossary _ _ 0.14.2 Special Vectors
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Glossary _ _ P C a , b ≡ XC YC ZC
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Glossary _ _ V ≡ V : = V • V Th
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Glossary _ _ 0.16.4 Matrix Partitio
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Glossary _ _ Only the subset of qua
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Glossary _ _ 0.19 Systeme Internati
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1 Chapter 1 / Introduction _ _ Chap
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Chapter 1 / Introduction _ _ Wherea
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Chapter 1 / Introduction _ _ • Cr
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Chapter 1 / Introduction _ _ genera
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Chapter 1 / Introduction _ _ radar
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Chapter 1 / Introduction _ _ simple
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Chapter 1 / Introduction _ _ optimi
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Chapter 1 / Introduction _ _ 1.3.9
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2 Chapter 2 / Target Modelling _ _
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Chapter 2 / Target Modelling _ _ 2.
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Chapter 2 / Target Modelling _ _
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Chapter 2 / Target Modelling _ _ t
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Chapter 2 / Target Modelling _ _ P&
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Chapter 2 / Target Modelling _ _ GO
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Chapter 2 / Target Modelling _ _ th
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Chapter 2 / Target Modelling _ _
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Chapter 2 / Target Modelling _ _ VX
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Chapter 2 / Target Modelling _ _ ma
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3 Chapter 3 / Sensors _ _ Chapter 3
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Chapter 3 / Sensors _ _ 3.1 Simulat
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Chapter 3 / Sensors _ _ Table 3-4 :
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Chapter 3 / Sensors _ _ Reference D
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Chapter 3 / Sensors _ _ 3.2-9 s s i
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Chapter 3 / Sensors _ _ 3.2-11 t o
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Chapter 3 / Sensors _ _ Figure 3-5
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Chapter 3 / Sensors _ _ Table 3-7 :
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Chapter 3 / Sensors _ _ IF ϕ LIM
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Chapter 3 / Sensors _ _ The phase e
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Chapter 3 / Sensors _ _ Taking expe
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Chapter 3 / Sensors _ _ Expressing
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Chapter 3 / Sensors _ _ INPUT; AA,
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Chapter 3 / Sensors _ _ The functio
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Chapter 3 / Inertial Navigation _ _
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Chapter 3 / Sensors / Gyroscopes _
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Chapter 3 / Sensors / Accelerometer
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Chapter 3 / Sensors / Barometric Al
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Chapter 3 / Sensors / Barometric Al
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Chapter 3 / Sensors / Radar Altimet
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Chapter 3 / Sensors / Radar _ _ 3.8
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Chapter 3 / Sensors / Radar _ _ LF
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Chapter 3 / Sensors / Radar _ _ ( )
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Chapter 3 / Sensors / Radar _ _ S :
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Chapter 3 / Sensors / Radar _ _ SN
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Chapter 3 / Sensors / Radar _ _ 2
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Chapter 3 / Sensors / Radar _ _ ⎛
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Chapter 3 / Sensors / Seeker _ _ 3.
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Chapter 3 / Sensors / Seeker _ _ 5
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Chapter 3 / Sensors / Seeker _ _ th
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Chapter 3 / Sensors / Seeker _ _ Th
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Chapter 3 / Sensors / Seeker _ _ Th
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Chapter 3 / Sensors / Fins _ _ 3.10
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Chapter 3 / Sensors / Fins _ _ thro
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Chapter 3 / Sensors / NAVSTAR GPS _
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Chapter 3 / Sensors / Helmet Mounte
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Chapter 3 / Sensors / Helmet Mounte
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Chapter 3 / Sensors / Air Data Syst
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Chapter 4 / Target Tracking _ _ 3.1
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Chapter 4 / Target Tracking _ _ Ine
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Chapter 4 / Target Tracking _ _ ran
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Chapter 5 / Missile State Observer
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5 Chapter 5 / Missile State Observe
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6 Chapter 6 / Missile Guidance _ _
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Chapter 6 / Missile Guidance _ _ 6.
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Chapter 6 / Missile Guidance _ _ As
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Chapter 6 / Missile Guidance _ _ CD
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Chapter 6 / Missile Guidance _ _ ge
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Chapter 6 / Missile Guidance _ _ ex
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Chapter 6 / Missile Guidance _ _ &
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Chapter 6 / Missile Guidance _ _ PN
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Chapter 6 / Missile Guidance _ _ ra
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Chapter 6 / Missile Guidance _ _ of
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Chapter 6 / Missile Guidance _ _ NO
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Chapter 6 / Missile Guidance _ _ tr
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Chapter 6 / Missile Guidance _ _ η
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Chapter 6 / Missile Guidance _ _ Au
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Chapter 6 / Missile Guidance _ _ Fo
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Chapter 11 / Future Research _ _ To
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References _ _ B.4 BAZARAA M.S., SH
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References _ _ F.1 FOX J.E., “A C
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References _ _ H.5 #HULL D.G., RADK
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References _ _ L.2 LOOZE D.P., HSU
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References _ _ N.4 NABAA N., BISHOP
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References _ _ R.3 RUSNACK I., “O
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References _ _ S.15 SINGER R.A.,
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References _ _ Y.2 YUAN P., CHERN J
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Bibliography _ _ B.13 BABA Y., YAMA
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Bibliography _ _ B.40 BECKER J.C.,
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Bibliography _ _ C.33 CORTINA E., O
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Bibliography _ _ E.8 ERSHOV A.A.,
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Bibliography _ _ G.34 GUTMAN P., VE
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Bibliography _ _ H.35 HUSSAIN A.M.,
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Bibliography _ _ K.14 KATZIR S., CL
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Bibliography _ _ L.19 LEFAS C.C,
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Bibliography _ _ M.16 MAYNE D.Q., P
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Bibliography _ _ P.1 PAINTER J.H.,
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Bibliography _ _ R.32 RONG LI X., Z
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Bibliography _ _ S.47 SPEYER J.L.,
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Bibliography _ _ V.5 VIAN J.L., MOO
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Bibliography _ _ W.29 WATSON G.A.,
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Appendix A / Geometric Points _ _ 1
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Appendix A / Geometric Points _ _ 1
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Appendix B / Frames of Reference _
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Appendix C / Axis Transforms _ _ 16
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Appendix C / Axis Transforms _ _ YP
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Appendix C / Axis Transforms _ _ B
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Appendix C / Axis Transforms _ _ YB
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Appendix C / Axis Transforms _ _ Us
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Appendix C / Axis Transforms _ _ No
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Appendix C / Axis Transforms _ _ B
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Appendix C / Axis Transforms _ _
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Appendix D / Point Mass Dynamics _
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Appendix E / Earth Geometry _ _ 18-
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Appendix E / Earth Geometry _ _ ELL
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Appendix E / Earth Geometry _ _ (dx
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Appendix E / Earth Geometry _ _ Int
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Appendix E / Earth Geometry _ _ 18.
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Appendix E / Earth Geometry _ _ 19-
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Appendix E / Earth Geometry _ _ P S
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Appendix E / Earth Geometry _ _ 19.
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Appendix E / Earth Geometry _ _ ∂
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Appendix G / Gravity _ _ 20-2
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Appendix G / Gravity _ _ g : = g +
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Appendix G / Gravity _ _ d −6 2
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Appendix G / Gravity _ _ 20-8
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Appendix H / Steady State Tracking
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Appendix I / Utilities _ _ 22.1-2
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Appendix I / Utilities _ _ Cartesia
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Appendix I / Utilities _ _ Matrix P
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Appendix I / Utilities _ _ 22.1-8
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Appendix I / Utilities / General Ut
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Appendix I / Utilities / WGS 84 Tar
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Appendix I / Utilities / Point Mass
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Appendix I / Utilities / Earth, Atm
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Appendix I / Utilities / Digital Fi
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Appendix I / Utilities / Matrices _
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Appendix I / Utilities / Quaternion
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