8–12 January 2018
Gaylord Palms, Kissimmee, Florida

Missile Guidance - NEW

6-7 January 2018

Synopsis

A system-level, integrated method is provided on missile guidance design, development, and system engineering activities in addressing requirements such as performance, cost, risk, and launch platform integration. The prediction methods presented are generally simple closed-form analytical expressions that are physics-based, to provide insight into the primary driving parameters. Typical values of missile guidance parameters and the characteristics of current operational missiles are discussed as well as the enabling subsystems and technologies for missile guidance and the current/projected state-of-the-art. Over forty videos illustrate missile guidance activities and performance.

Key Topics

  • Key drivers in the missile guidance design and system engineering process
  • Critical tradeoffs, methods, and technologies in missile guidance sizing
  • Targeting system, launch platform, and-missile guidance integration
  • Missile guidance sizing examples
  • Missile guidance system and technology development process

Who Should Attend

The course is oriented toward the needs of missile engineers, system engineers, system analysts, marketing personnel, program managers, university professors, and others working in the area of missile guidance systems and missile guidance technology development. Attendees will gain an understanding of missile guidance design, missile guidance technologies, targeting and launch platform integration, missile guidance measures of merit, and the missile guidance system development process.

Instructor

Eugene L. Fleeman has 50+ years of government, industry, academia, and consulting experience in the design and development of missile systems. Formerly a manager of missile programs at the US Air Force Research Laboratory, Rockwell International, Boeing, and Georgia Tech, he is an international lecturer on missiles and the author of 200+ publications, including three textbooks. His textbooks and short courses on Missile Design, Development, and System Engineering emphasize physics-based prediction methods, for enhanced insight, speed, and accuracy to the conceptual design process. Since the year 1999 his short courses have been held in fifteen countries and five continents. Additional information is available at the web site.

Outline

  • Introduction/Drivers in Missile Guidance
  • Aerodynamic Considerations in Missile Guidance
    • Flight control alternatives, including tail, canard, wing, thrust vector, and reaction jet control
    • Guidelines for missile stability and flight control effectiveness
    • Conceptual design methods for predicting missile maneuverability and off-boresight
    • Comparisons of missile maneuver laws
  • Weight Considerations in Missile Guidance
    • Conceptual design methods for predicting the weight of missile guidance, radome, power supply and actuators
  • Flight Performance Considerations in Missile Guidance
    • Conceptual design methods for predicting missile maneuverability and off-boresight
    • Equations of motion and drivers for missile guidance
  • Other Measures of Merit and Launch Platform Integration/System Engineering
    • Navigation alternatives, including Global Positioning Satellite (GPS), inertial reference, terrain contour matching (TERCOM), and digital scene matching
    • Seeker/sensor/data link alternatives including radar, infrared, and laser
    • Conceptual design methods for predicting the range and tracking accuracy of seekers and seeker domes
    • Seeker robustness considerations, including performance with adverse weather, clutter, automatic target recognition, and countermeasures
    • Impact of measures of merit for robustness, lethality, accuracy, observables, reliability, and cost on missile guidance
    • Carriage interfaces, fire control interfaces, and environmental requirements for aircraft, ground vehicle, and ship launch platforms
    • Comparisons of terminal guidance alternatives
  • Example of Aerodynamic Sizing to Meet Guidance Accuracy Requirement
    • Design, build, and fly (DBF) competition. Each student will design, build, and fly their individual soda straw rockets
    • Simplified illustration of the missile development process, Pareto sensitivity analysis, uncertainty analysis, House of Quality (HOQ), and Design of Experiment (DOE)
  • Missile Guidance Development Process
    • Guidance simulation including conceptual design modeling, preliminary design modeling, six-degrees of freedom digital modeling, and hardware-in-loop modeling
    • Missile guidance development process, facilities, and development tests
    • New technologies for missile guidance
  • Some Lessons Learned
  • Summary
  • References and Follow-up Communication
  • Appendices (Homework Problems/Classroom Exercises, Example of Request for Proposal, Nomenclature, Acronyms, Conversion Factors, Syllabus, Quizzes, Design Case Studies, TMD Spreadsheet, Soda Straw Rocket Science)

Course Materials

Course notes will be made available about one week prior to the course event. You will receive an email with detailed instructions on how to access your course notes. Since these notes will not be distributed on site, AIAA and your course instructor highly recommend that you bring your computer with the course notes already downloaded.

Course Registration

Pricing and registration information can be found here.

Contact

Please contact Jason Cole if you have any questions about courses and workshops at AIAA forums.

Dates to Remember

  • Manuscript Deadline: 05 Dec 2017
  • Early Bird Reg Deadline: 18 Dec 2017
  • Cancellation Deadline: 18 Dec 2017

FAQsContact UsPoliciesMedia