Flight Dynamics and Control 1 (AEM 368)

AEM 368 is an introduction to aircraft dynamics including performance and stability and control. Dr. O’Neill taught this course in the Spring of 2017.Example Lectures:

Required Books:

  • Flight Stability and Automatic Control, R. Nelson, McGraw-Hill, 2nd ed, 1998.
  • Aircraft Performance and Design, John Anderson, McGraw-Hill, 1999.

Goals:

By the end of the course, students should be able to:

  • Understand basic aircraft performance and stability and control (S&C) terminology
  • Estimate aircraft performance in steady and accelerated flight mission phases
  • Size S&C surfaces of an aircraft
  • Demonstrate a physical and mathematical understanding of aircraft flight modes

Topics:

We will cover S&C and performance topics in the textbooks. Selected topics and sources supplement the text.

  • Aircraft Nomenclature, Atmosphere, Instruments
  • Static stability and control (FSAC, Chap 1)
  • Aircraft equations of motion (FSAC, Chap 2)
  • Longitudinal motion (FSAC, Chap 3)
  • Lateral motion (FSAC, Chap 4)
  • Steady Flight (APD, Chap 5)
  • Accelerated Flight (APD, Chap 6)
  • Aircraft Performance and Control Projects

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