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

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Bibliography _ _ W.29 WATSON G.A., BLAIR W.D., “Interacting Acceleration Compensation Algorithm for Tracking Maneuvering Targets”, IEEE AES, Vol. 31, No. 3, 1995, pp. 1152-1158. X.1 XIHENG H., “FF-Pade Method of Model Reduction in Frequency Domain”, IEEE AC., Vol. 32, No. 3, pp. 243-248. Y.10 YAKOWITZ S.J., “The Stagewise Kuhn-Tucker Condition and Differential Dynamic Programming”, IEEE AC., Vol. 31, No. 1, 1986, pp. 25-67. Y.11 YANG S.M., “Analysis of Optimal Midcourse Guidance Law”, IEEE AES, Vol. 32, No. 1, 1996, pp. 419-425. Y.12 YANG C-D., YANG C-C., “Optimal Pure Proportional Navigation for Maneuvering Targets”, IEEE AES, Vol. 33, No. 3, 1997, pp. 949-957. Y.13 YANG Z., “Partical Velocity Estimation Using Kalman Filtering”, IEEE AES, Vol. 21, No. 3, 1985, pp. 407-419. Y.14 YUEH W.R., LIN C., “Guidance Performance Analysis with In-Flight Radome Error Calibration”, AIAA J. Guidance and Control, Vol. 8, No. 5, 1985, pp. 666-669. Z.4 ZELINSKI A., KLEINLE B., “Design of a Minature High Precision Ovenised Oscillator for GPS Receivers”, J. ION, Vol. 36, No. 4, pp. 379- 395. Z.5 ZHU Y., “Efficient Recursive State Estimator for Dynamic Systems without Knowledge of Noise Covariances”, IEEE AES, Vol. 35, No. 1, 1999, pp. 102-113. Z.6 ZHUANG W., TRANQUILLA J., “Modeling and Analysis for the GPS Pseudo-Range Observable”, IEEE AES, Vol. 31, No. 2, pp. 739-751. 13-28 X Y Z
AppendixA / Geometric Points _ _ APPENDIX A 14 GEOMETRIC POINTS The Glossary reflects the breadth of the work undertaken and imposes a common framework within which algorithms from various disciplines can be expressed. The generic nature of the definitions therein, and their relationship with the naming convention adopted for simulation work, must be customised, starting with the definition of the critical points associated with the air defence application. The geometric points defined here are usually associated with the origin of the Frames-of-Reference dealt with in Appendix B. Although terrestrial vehicle dynamics are the main consideration, the use of inertial motion sensors, and a GPS constellation, means that an inertial reference must be established for long-range vehicles; a reference which provides a general platform for dynamics of a point with respect to inertial space. Only the geometrical points listed in Table 14-1 are used when defining vectors. When selecting notation for geometric points (i , j , k) are reserved for use as mathematical indices. 14-1
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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 _ _
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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 _ _
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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 6 / Missile Guidance _ _ (
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Chapter 6 / Missile Guidance _ _
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Chapter 6 / Missile Guidance _ _ ar
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7 Chapter 7 / Missile Trajectory Op
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Chapter 7 / Missile Trajectory Opti
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8 Chapter 8 / Simulation _ _ Chapte
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Chapter 8 / Simulation _ _ 8.1 The
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Chapter 8 / Simulation _ _ 8.3 The
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Chapter 8 / Simulation _ _ Having p
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Chapter 8 / Simulation _ _ 8.5.1 Gl
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Chapter 8 / Simulation _ _ (1) CONS
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Chapter 8 / Simulation _ _ 8.6.2 Ou
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Chapter 8 / Simulation _ _ The file
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Chapter 8 / Simulation _ _ • The
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Chapter 8 / Simulation _ _ comprehe
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Chapter 8 / Simulation _ _ WIN_RATE
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Chapter 8 / Simulation _ _ for this
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Chapter 8 / Simulation _ _ with the
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Chapter 8 / Simulation _ _ Figure 8
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Chapter 8 / Simulation _ _ Table 8-
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Chapter 8 / Simulation _ _ 8.8 Disc
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9 Chapter 9 / Performance _ _ Chapt
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Chapter 9 / Performance _ _ 9.1 Air
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Chapter 9 / Performance _ _ XM ( >
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Chapter 9 / Performance _ _ 9.3 PN
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Chapter 9 / Performance _ _ The eff
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Chapter 9 / Performance _ _ VXMVOM
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Chapter 9 / Performance _ _ VXMVOM
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Chapter 9 / Performance _ _ 9.4 CLO
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Chapter 9 / Performance _ _ AR_BOM
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Chapter 9 / Performance Chapter 9 /
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Initially the position error falls
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values of CN are not always a relia
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crude initialisation introduces err
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9.5.3 Singer Filter Tuning The Sing
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9.6.2 CLOS Study The CLOS study sho
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Chapter 10 / Conclusions _ _ 10-2
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Chapter 10 / Conclusions _ _ 10.3 T
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Page 436 and 437: References _ _ B.4 BAZARAA M.S., SH
Page 438 and 439: References _ _ F.1 FOX J.E., “A C
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Page 448 and 449: References _ _ S.15 SINGER R.A.,
Page 450 and 451: References _ _ Y.2 YUAN P., CHERN J
Page 452 and 453: Bibliography _ _ B.13 BABA Y., YAMA
Page 454 and 455: Bibliography _ _ B.40 BECKER J.C.,
Page 456 and 457: Bibliography _ _ C.33 CORTINA E., O
Page 458 and 459: Bibliography _ _ E.8 ERSHOV A.A.,
Page 460 and 461: Bibliography _ _ G.34 GUTMAN P., VE
Page 462 and 463: Bibliography _ _ H.35 HUSSAIN A.M.,
Page 464 and 465: Bibliography _ _ K.14 KATZIR S., CL
Page 466 and 467: Bibliography _ _ L.19 LEFAS C.C,
Page 468 and 469: Bibliography _ _ M.16 MAYNE D.Q., P
Page 470 and 471: Bibliography _ _ P.1 PAINTER J.H.,
Page 472 and 473: Bibliography _ _ R.32 RONG LI X., Z
Page 474 and 475: Bibliography _ _ S.47 SPEYER J.L.,
Page 476 and 477: Bibliography _ _ V.5 VIAN J.L., MOO
Page 480 and 481: Appendix A / Geometric Points _ _ 1
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Page 484 and 485: Appendix B / Frames of Reference _
Page 494 and 495: Appendix C / Axis Transforms _ _ 16
Page 496 and 497: Appendix C / Axis Transforms _ _ YP
Page 498 and 499: Appendix C / Axis Transforms _ _ B
Page 500 and 501: Appendix C / Axis Transforms _ _ YB
Page 504 and 505: Appendix C / Axis Transforms _ _ Us
Page 506 and 507: Appendix C / Axis Transforms _ _ No
Page 508 and 509: Appendix C / Axis Transforms _ _ B
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Page 514 and 515: Appendix D / Point Mass Dynamics _
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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 / WGS 84 Tar
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Appendix I / Utilities / Digital Ma
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Appendix I / Utilities / Digital Fi
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Appendix I / Utilities / Quaternion
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