1/9/2009 ELF 1

Outline

Introduction / Key Drivers in the Missile Design and Integration Process

Aerodynamic Considerations in Missile Design and Integration

Propulsion Considerations in Missile Design and Integration

Weight Considerations in Missile Design and Integration

Flight Performance Considerations in Missile Design and Integration

Measures of Merit and Launch Platform Integration

Sizing Examples

Development Process

Summary and Lessons Learned

References and Communication

Appendices ( Homework Problems / Classroom Exercises, Example of

Request for Proposal, Nomenclature, Acronyms, Conversion Factors,

Syllabus )

1/9/2009 ELF 2

Evaluate Alternatives and Iterate the

System-of-Systems Design

• Mission / Scenario

/ System Definition

• Weapon System

Requirements,

Trade Studies

and Sensitivity

Analysis

• Launch Platform

Integration

• Weapon Concept

Design Synthesis

• Technology

Assessment and

Dev Roadmap

Initial

Tech

Initial

Reqs

Baseline

Selected

Alt

Concepts

Initial Carriage /

LaunchIteration

Refine

Weapons

Req

Initial Revised

Trades / Eval Effectiveness / Eval

Tech

Trades

Initial

Roadmap

Revised

Roadmap

Update

Note: Typical design cycle for conceptual design is usually 3 to 9 months

Alternate Concepts Select Preferred Design Eval / Refine

1/9/2009 ELF 3

Exploit Diverse Skills for a Balanced Design

Customer ( requirements pull )

mission / MIR weighting

Operations analysts

system-of-systems analysis

System integration engineers

launch platform integration

Missile design engineers

missile concept synthesis

Technical specialists ( technology push )

technology assessment / roadmap

1/9/2009 ELF 4

Utilize Creative Skills

Use Creative Skills to Consider Broad Range of Alternatives

Ask Why? of Requirements / Constraints

Project into Future ( e.g., 5 – 15 years )

State-of-the-art ( SOTA )

Threat

Scenario / Tactics / Doctrine

Concepts

Technology Impact Forecast

Recognize and Distill the Most Important, Key Drivers

Develop Missile Concept that is Synergistic within a

System-of-Systems

Develop Synergistic / Balanced Combination of High

Leverage Subsystems / Technologies

1/9/2009 ELF 5

Identify, Quantify, and Balance the Cost Effective Measures of Merit

Max / MinRange

Time to

TargetRobustness

WeightSurvivability

Lethality Miss Distance

Observables

Reliability

1/9/2009 ELF 6

Start with a Good Baseline

I would have

used the wheel

as a baseline.

Evaluate Prediction Methods for Uncertainty in

Accuracy and Precision

1/9/2009 ELF 7

Precision

Accuracy

1/9/2009 ELF 8

Conduct Balanced, Unbiased Trade-offs

Aerodynamics

Propulsion

Structures

Seeker

Guidance and

Control

Warhead – Fuze

Production

1/9/2009 ELF 9

AA- 8 / R-60 Python 4 Magic 550 U-Darter

Python 5 Derby / R-Darter AIM-9L Aspide

AA-10 / R-27 Skyflash AIM-7 R-37

AA-12 / R-77 AIM-9x Super 530D AIM-132

AA-11 / R-73 SD-10 / PL12 AIM-120 Mica

IRIS-T Meteor A-Darter Taildog

Evaluate Many Alternatives

Note: Although all of the above are supersonic air-to-air missiles, they have different configuration geometry

1/9/2009 ELF 10

Search a Broad Design Solution Space

( Global Optimization vs Local Optimization )

Local Optimum ( e.g., Lowest Cost Only in Local Solution Space )

Local Optimum ( e.g., Lowest Cost Only in Local Solution Space )

Global Optimum ( e.g., Lowest Cost in Global Solution Space ) within Constraints

1/9/2009 ELF 11

Evaluate and Refine as Often as Possible

1/9/2009 ELF 12

Provide Balanced Emphasis of

Analytical vs Experimental

Thomas Edison: "Genius is 1% inspiration and 99% perspiration."

Albert Einstein: "The only real valuable thing is intuition."

1/9/2009 ELF 13

Use Design, Build, and Fly Process, for Feedback

Leading to Broader Knowledge / Understanding

Design

Build

Fly ( Test )

Prediction Satisfies

Customer

Requirements?

Test Results Satisfy

Customer Requirements

and Consistent with

Prediction?

Is it Producible?

No

Yes

Data

Failure / Success

Information

Understanding

Wisdom

No

No

Where is the wisdom we have lost in knowledge? Where is the knowledge we have lost in information?--T. S. Eliot ( The Rock )

Knowledge comes by taking things apart: analysis. But wisdom comes by putting things together.--John A. Morrison

We are drowning in information but starved for knowledge.--John Naisbitt ( Megatrends: Ten New Directions Transforming Our Lives )

We learn wisdom from failure much more than from success. We often discover what will do, by finding out what will not do; and probably he who never made a mistake never made a discovery.--Samuel Smiles ( Self Help )

Knowledge

1/9/2009 ELF 14

Consider Follow-on Consequences of Decisions -Actions Have Consequences

1/9/2009 ELF 15

Keep Track of Assumptions and Develop

Real-Time Documentation

It’s finally

finished ! . . .

1/9/2009 ELF 16

Develop Good Documentation

Mission flight profiles of

preferred concept( s )

1/9/2009 ELF 17

Effectively Utilize Conceptual Design Group Skills

- Maximize Strengths and Minimize Weaknesses

Source: Nicolai, L.M., “Designing a Better Engineer,” AIAA Aerospace America, April 1992

Detail /

Production

Design –

30%

Other Than

Design –

60%

Preliminary Design – 8%Conceptual Design – 2%

(Test, Analysis,

Configuration

Management, Software,

Program Management,

Integration,

Requirements,

etc.)

1/9/2009 ELF 18

Balance the Trade-off of

Importance Versus Priority

Advanced Programs /

Conceptual Design

SDD Programs /

Preliminary Design

Production Programs /

Detail Design

1/9/2009 ELF 19

Evaluate Alternatives and Iterate the

Configuration Design

Yes

Establish Baseline

Meet

Performance?

No

No

Yes

Resize / Alt Config / Subsystems / Tech

Alt Mission

Alt Baseline

Define Mission Requirements

Aerodynamics

Propulsion

Weight

Trajectory

Measures of Merit and Constraints

1/9/2009 ELF 20

Configuration Sizing Conceptual Design

Guidelines: Aeromechanics

Configuration Sizing Parameter Aeromechanics Design Guideline Body fineness ratio 5 < l / d < 25

Nose fineness ratio lN / d 2 if M > 1

Boattail or flare angle < 10 deg

Efficient cruise dynamic pressure q < 1,000 psf

Missile homing velocity VM / VT > 1.5

Ramjet combustion temperature > 4,000 F

Oblique shocks prior to inlet normal > 2 oblique shocks / compressions if M > shock to satisfy MIL-E-5008B 3.0, > 3 shocks / compressions if M > 3.5

Inlet flow capture Shock on cowl lip at Mmax cruise

Ramjet Minimum cruise Mach number M > 1.2 x MInletStart , M > 1.2 MMaxThrust = Drag

Subsystems packaging Maximize available volume for fuel / propellant

1/9/2009 ELF 21

Configuration Sizing Conceptual Design

Guidelines: Guidance & Control

Configuration Sizing Parameter G&C Design Guideline

Body bending frequency BB > 2 ACT

Trim control power / > 1

Neutral stability tail-body If low aspect ratio, b / d 2, c / d > 1

Stability & control cross coupling < 30%

Airframe time constant < 0.2 s

Missile maneuverability nM / nT > 3

Proportional guidance ratio 3 < N’ < 5

Target span resolution by seeker < btarget

Missile heading rate .M >

.T

Missile turn radius RTM< RTT

1/9/2009 ELF 22

Wrap Up ( Part 1 of 2 )

Missile Design Is a Creative and Iterative Process that Includes

System integration considerations

Missile concepts and sizing

Technology assessment

Flight trajectory evaluation

Measures of merit evaluation

Cost / Performance / Risk Drivers Often “Locked In” During

Conceptual Design

Missile Design Is Best Conducted by a Diverse Group

Military customer mission / scenario definition

Operations analysts system-of-systems modeling

System integration engineers launch platform integration

Missile design engineers missile concept synthesis

Technical specialists technology assessment / technology roadmap

1/9/2009 ELF 23

Wrap Up ( Part 2 )

The Missile Conceptual Design Philosophy Requires

Iteration, iteration, iteration

Evaluation of a broad range of alternatives

Traceable flow-down allocation of requirements

Starting with a good baseline

Pareto sensitivity analysis to determine most important, driving

parameters

Synergistic compromise / balanced subsystems and technologies

that are high leverage

Awareness of technology SOTA / technology assessment

Technology impact forecast

Robust design

Creative design decisions made by the designer ( not the computer )

Fast, simple, robust, physics-based prediction methods

1/9/2009 ELF 24

Outline

Introduction / Key Drivers in the Missile Design and Integration Process

Aerodynamic Considerations in Missile Design and Integration

Propulsion Considerations in Missile Design and Integration

Weight Considerations in Missile Design and Integration

Flight Performance Considerations in Missile Design and Integration

Measures of Merit and Launch Platform Integration

Sizing Examples

Development Process

Summary and Lessons Learned

References and Communication

Appendices ( Homework Problems / Classroom Exercises, Example of

Request for Proposal, Nomenclature, Acronyms, Conversion Factors,

Syllabus )

1/9/2009 ELF 25

References

1. “Missile.index,” http://missile.index.ne.jp/en/

2. AIAA Aerospace Design Engineers Guide, American Institute of Aeronautics and Astronautics, 1993

3. Bonney, E.A., et al, Aerodynamics, Propulsion, Structures, and Design Practice, “Principles of Guided Missile Design”,

D. Van Nostrand Company, Inc., 1956

4. Jerger, J.J., Systems Preliminary Design Principles of Guided Missile Design, “Principles of Guided Missile Design”, D.

Van Nostrand Company, Inc., 1960

5. Chin, S.S., Missile Configuration Design, McGraw-Hill Book Company, 1961

6. Mason, L.A., Devan, L., and Moore, F.G., “Aerodynamic Design Manual for Tactical Weapons,” NSWCTR 81-156, 1981

7. Pitts, W.C., Nielsen, J.N., and Kaattari, G.E., “Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic,

Transonic, and Supersonic Speeds,” NACA Report 1307, 1957

8. Jorgensen, L.H., “Prediction of Static Aerodynamic Characteristics for Space-Shuttle-Like, and Other Bodies at Angles

of Attack From 0 to 180,” NASA TND 6996, January 1973

9. Hoak, D.E., et al., “USAF Stability and Control DATCOM,” AFWAL TR-83-3048, Global Engineering, 1978

10. “Nielsen Engineering & Research (NEAR) Aerodynamic Software Products,” http://www.nearinc.com/near/software.htm

11. Durham, F. P., Aircraft Jet Powerplants, Prentice-Hall, 1961

12. Ashley, H., Engineering Analysis of Flight Vehicles, Dover Publications, Inc., 1974

13. Anderson, J.D. Jr., “Modern Compressible Flow,” Second Edition, McGraw Hill, 1990

14. Kinroth, G.D. and Anderson, W.R., “Ramjet Design Handbook,” CPIA Pub. 319 and AFWAL TR 80-2003, June 1980

15. “Technical Aerodynamics Manual,” North American Rockwell Corporation, DTIC AD 723823, June 1970

16. Oswatitsch, K.L., “Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds”, NACA TM -

1140, 1947

17. Carslaw, H.S. and Jaeger, J. C., Conduction of Heat in Solids, Clarendon Press, 1988

1/9/2009 ELF 26

References ( cont )

18. Allen, J. and Eggers, A.J., “A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth’s

Atmosphere at High Supersonic Speeds”, NACA Report 1381, April 1953

19. Levens, A.S., Nomography, John Wiley & Sons, 1937

20. Schneider, S.H., Encyclopedia of Climate and Weather, Oxford University Press, 1996

21. Klein, L.A., Millimeter-Wave and Infrared Multisensor Design and Signal Processing, Artech House, Boston, 1997

22. US Army Ordnance Pamphlet ORDP-20-290-Warheads, 1980

23. Taylor, G.I., “The Formation of a Blast Wave by a Very Intense Explosion,. Part I. Theoretical Discussion”,

Proceedings of the Royal Society of London, Vol. 201, March 1950

23. Carleone, J. (Editor), Tactical Missile Warheads, “AIAA Vol. 155 Progress in Astronautics and Aeronautics,” American

Institute of Aeronautics and Astronautics, 1993

24. Christman, D.R. and Gehring, J.W., “Analysis of High-Velocity Projectile Penetration Mechanics,” Journal of Applied

Physics, Vol. 37, 1966

25. Heaston, R.J. and Smoots, C.W., “Precision Guided Munitions,” GACIAC Report HB-83-01, May 1983

26. Donatelli, G.A. and Fleeman, E.L., “Methodology for Predicting Miss Distance for Air Launched Missiles,” AIAA-82-

0364, January 1982

27. Bennett, R.R. and Mathews, W.E., “Analytical Determination of Miss Distances for Linear Homing Navigation Systems,”

Hughes Tech Memo 260, 31 March 1952

28. Crispin, J. W., Jr., Goodrich, R. F., and Siegel, K. M., “A Theoretical Method for the Calculation of the Radar Cross

Section of Aircraft and Missiles,” University of Michigan Report 2591-1-H, July 1959

29. Nicholas, T. and Rossi, R., “US Missile Data Book, 1999,” Data Search Associates, 1999

30. Cengel, Y. A., Heat and Mass Transfer: A Practical Approach, McGraw-Hill, 2006

31. Jarvinen, P. O., and Hill, J. A. F., “Universal Model for Underespanded Rocket Plumes in Hypersonic Flow”,

Proceedings of the 12th JANAF Liquid Propulsion Meeting, Nov. 1970

1/9/2009 ELF 27

References ( cont )

32. Bithell, R.A. and Stoner, R.C., “Rapid Approach for Missile Synthesis,” AFWAL TR 81-3022, March 19822.

33. Fleeman, E.L. and Donatelli, G.A., “Conceptual Design Procedure Applied to a Typical Air-Launched Missile,” AIAA 81-

1688, August 1981

34 Hindes, J.W., “Advanced Design of Aerodynamic Missiles ( ADAM ),“ October 1993

35. Frits, A.P., et al, “A Conceptual Sizing Tool for Tactical Missiles, “ AIAA Missile Sciences Conference, November 2002

36. Bruns, K.D., Moore, M.E., Stoy, S.L., Vukelich, S.R., and Blake, W.B., “Missile DATCOM,” AFWAL-TR-91-3039, April

1991

37. Moore, F.G., et al, “The 2002 Version of the Aeroprediction Code”, Naval Surface Warfare Warfare Center, March 2002

38. Nicolai, L.M., “Designing a Better Engineer,” AIAA Aerospace America, April 1992

1/9/2009 ELF 28

Bibliography of Other Reports and Web Sites

System Design

Fleeman, E.L., Tactical Missile Design, 2nd Edition, American Institute of Aeronautics and Astronautics, 2006

“DoD Index of Specifications and Standards,” http://stinet.dtic.mil/str/dodiss.html

“Periscope,” http://www.periscope1.com/

Defense Technical Information Center, http://www.dtic.mil/

NATO Research & Technology Organisation, http://www.rta.nato.int/

“Missile System Flight Mechanics,” AGARD CP270, May 1979

Hogan, J.C., et al., “Missile Automated Design ( MAD ) Computer Program,” AFRPL TR 80-21, March 1980

Rapp, G.H., “Performance Improvements With Sidewinder Missile Airframe,” AIAA Paper 79-0091, January 1979

Nicolai, L.M., Fundamentals of Aircraft Design, METS, Inc., 1984

Lindsey, G.H. and Redman, D.R., “Tactical Missile Design,” Naval Postgraduate School, 1986

Lee, R.G., et al, Guided Weapons, Third Edition, Brassey’s, 1998

Giragosian, P.A., “Rapid Synthesis for Evaluating Missile Maneuverability Parameters,” 10th AIAA Applied

Aerodynamics Conference, June 1992

Fleeman, E.L. “Aeromechanics Technologies for Tactical and Strategic Guided Missiles,” AGARD Paper

presented at FMP Meeting in London, England, May 1979

Raymer, D.P., Aircraft Design, A Conceptual Approach, American Institute of Aeronautics and Astronautics, 1989

Ball, R.E., The Fundamentals of Aircraft Combat Survivability Analysis and Design, American Institute of

Aeronautics and Astronautics, 1985

“National Defense Preparedness Association Conference Presentations,” http://www.dtic.mil/ndia

1/9/2009 ELF 29

Bibliography of Other Reports and Web Sites ( cont )

System Design ( continued )

Eichblatt, E.J., Test and Evaluation of the Tactical Missile, American Institute of Aeronautics and Astronautics,

1989

“Aircraft Stores Interface Manual (ASIM),” http://akss.dau.mil/software/1.jsp

“Advanced Sidewinder Missile AIM-9X Cost Analysis Requirements Description (CARD),”

http://deskbook.dau.mil/jsp/default.jsp

Wertz, J.R and Larson W.J., Space Mission Analysis and Design, Microprism Press and Kluwer Academic Publishers, 1999

“Directory of U.S. Military Rockets and Missiles”, http://www.designation-systems.net/

Fleeman, E.L., et al, “Technologies for Future Precision Strike Missile Systems,” NATO RTO EN-018, July 2001

“The Ordnance Shop”, http://www.ordnance.org/portal/

“Conversion Factors by Sandelius Instruments”, http://www.sandelius.com/reference/conversions.htm

“Defense Acquisition Guidebook”, http://akss.dau.mil/dag/

“Weaponry”, http://www.deagel.com/

Aerodynamics

“A Digital Library for NACA,” http://naca.larc.nasa.gov/

Briggs, M.M., Systematic Tactical Missile Design, Tactical Missile Aerodynamics: General Topics, “AIAA Vol. 141

Progress in Astronautics and Aeronautics,” American Institute of Aeronautics, 1992

Briggs, M.M., et al., “Aeromechanics Survey and Evaluation, Vol. 1-3,” NSWC/DL TR-3772, October 1977

“Missile Aerodynamics,” NATO AGARD LS-98, February 1979

“Missile Aerodynamics,” NATO AGARD CP-336, February 1983

“Missile Aerodynamics,” NATO AGARD CP-493, April 1990

“Missile Aerodynamics,” NATO RTO-MP-5, November 1998

Nielsen, J.N., Missile Aerodynamics, McGraw-Hill Book Company, 1960

1/9/2009 ELF 30

Bibliography of Other Reports and Web Sites ( cont )

Aerodynamics ( continued )

Mendenhall, M.R. et al, “Proceedings of NEAR Conference on Missile Aerodynamics,” NEAR, 1989

Nielsen, J.N., “Missile Aerodynamics – Past, Present, Future,” AIAA Paper 79-1818, 1979

Dillenius, M.F.E., et al, “Engineering-, Intermediate-, and High-Level Aerodynamic Prediction Methods and

Applications,” Journal of Spacecraft and Rockets, Vol. 36, No. 5, September-October, 1999

Nielsen, J.N., and Pitts, W.C., “Wing-Body Interference at Supersonic Speeds with an Application to

Combinations with Rectangular Wings,” NACA Tech. Note 2677, 1952

Spreiter, J.R., “The Aerodynamic Forces on Slender Plane-and Cruciform-Wing and Body Combinations”, NACA

Report 962, 1950

Simon, J.M., et al, “Missile DATCOM: High Angle of Attack Capabilities, AIAA-99-4258

Burns, K.A., et al, “Viscous Effects on Complex Configurations,” WL-TR-95-3060, 1995

Lesieutre, D., et al, “Recent Applications and Improvements to the Engineering-Level Aerodynamic Prediction

Software MISL3,’’ AIAA-2002-0274

Moore, F.G., Approximate Methods for Weapon Aerodynamics, American Institute of Aeronautics and

Astronautics, 2000

“1976 Standard Atmosphere Calculator,” http://www.digitaldutch.com/atmoscalc/

“Compressible Aerodynamics Calculator,” http://www.aoe.vt.edu/~devenpor/aoe3114/calc.html

Ashley, H. and Landahl, M., Aerodynamics of Wings and Bodies, Dover Publications, 1965

John, James E.A., Gas Dynamics, Second Edition, Prentice Hall, 1984

Zucker, Robert D., Fundamentals of Gas Dynamics, Matrix Publishers, 1977

Propulsion

Chemical Information Propulsion Agency, http://www.cpia.jhu.edu/

St. Peter, J., The History of Aircraft Gas Turbine Engine Development in the United States: A Tradition of Excellence, ASME International Gas Turbine Institute, 1999

1/9/2009 ELF 31

Bibliography of Other Reports and Web Sites ( cont )

Propulsion ( continued )

Mahoney, J.J., Inlets for Supersonic Missiles, American Institute of Aeronautics and Astronautics, 1990

Sutton, G.P., Rocket Propulsion Elements, John Wiley & Sons, 1986

“Tri-Service Rocket Motor Trade-off Study, Missile Designer’s Rocket Motor handbook,” CPIA 322, May 1980

Humble, R.W., Henry, G.N., and Larson, W.J., Space Propulsion Analysis and Design, McGraw-Hill, 1995

Jenson, G.E. and Netzer, D.W., Tactical Missile Propulsion, American Institute of Aeronautics and Astronautics,

1996

Durham, F.P., Aircraft Jet Powerplants, Prentice-Hall, 1961

Bathie, W.W., Fundamentals of Gas Turbines, John Wiley and Sons, 1996

Hill, P.G. and Peterson, C.R., Mechanics and Thermodynamics of Propulsion, Addison-Weshley Publishing Company, 1970

Mattingly, J.D., et al, Aircraft Engine Design, American Institute of Aeronautics and Astronautics, 1987

Materials and Heat Transfer

Budinski, K.G. and Budinski, M.K., Engineering Materials Properties and Selection, Prentice Hall, 1999

“Matweb’s Material Properties Index Page,” http://www.matweb.com

“NASA Ames Research Center Thermal Protection Systems Expert (TPSX) and Material Properties Database”,

http://tpsx.arc.nasa.gov/tpsxhome.shtml

Harris, D.C., Materials for Infrared Windows and Domes, SPIE Optical Engineering Press, 1999

Kalpakjian, S., Manufacturing Processes for Engineering Materials, Addison Wesley, 1997

MIL-HDBK-5J, “Metallic Materials and Elements for Aerospace Vehicle Structures”, Jan 2003

“Metallic Material Properties Development and Standardization ( MMPDS )”, http://www.mmpds.org

1/9/2009 ELF 32

Bibliography of Other Reports and Web Sites ( cont )

Materials and Heat Transfer ( continued )

Mallick, P.K., Fiber-Reinforced Composites: Materials, Manufacturing, and Design, Second Edition, Maecel

Dekker, 1993

Chapman, A.J., Heat Transfer, Third Edition, Macmillan Publishing Company, 1974

Incropera, F.P. and DeWitt, D.P., Fundamentals of Heat and Mass Transfer, Fourth Edition, John Wiley and Sons,

1996

Guidance, Navigation, Control, and Sensors

Zarchan, P., Tactical and Strategic Missile Guidance, AIAA Vol. 124 Progress in Astronautics and Aeronautics,

American Institute of Aeronautics and Astronautics, 1990

“Proceedings of AGARD G&C Conference on Guidance & Control of Tactical Missiles,” AGARD LS-52, May 1972

Garnell, P., Guided Weapon Control Systems, Pergamon Press, 1980

Locke, A. S., Guidance, Principles of Guided Missile Design, D. Van Nostrand, 1955

Blakelock, J. H., Automatic Control of Aircraft and Missiles, John Wiley & Sons, 1965

Lawrence, A.L., Modern Inertial Technology, Springer, 1998

Siouris, G.M., Aerospace Avionics Systems, Academic Press, 1993

Stimson, G.W., Introduction to Airborne Radar, SciTech Publishing, 1998

Lecomme, P., Hardange, J.P., Marchais, J.C., and Normant, E., Air and Spaceborne Radar Systems, SciTech

Publishing and William Andrew Publishing, 2001

Wehner, D.R., High-Resolution Radar, Artech House, Norwood, MA, 1995

Donati, S., Photodetectors, Prentice-Hall, 2000

Jha, A.R., Infrared Technology, John Wiley and Sons, 2000

Schlessinger, M., Infrared Technology Fundamentals, Marcel Decker, 1995

Skolnik, M.I., Introduction to Radar Systems, McGraw-Hill, 1980

Hovanessian, S.A., Radar Detection and Ranging Systems, Artech House, 1973

1/9/2009 ELF 33

Bibliography of Other Reports and Web Sites ( cont )

Guidance, Navigation, Control, and Sensors ( continued )

Moir, I., and Seavridge, A., Military Avionics Systems, American Institute of Aeronautics and Astronautics, 2006

Mahafza, B. A., Radar Systems Analysis and Design Using MATLAB ® , 2nd Edition, Chapman & Hall / CRC, 2005

1/9/2009 ELF 34

Follow-up Communication

I would appreciate receiving your comments and

corrections on this presentation, as well as any data,

examples, or references that you may offer.

Thank you,

Gene Fleeman

Tactical Missile Design

E-mail: GeneFleeman@msn.com

Web Site: http://genefleeman.home.mindspring.com