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Missile Autopilot Design Techniques by Dpt Htegn is a document available to read on EtoBox.

What is Missile Autopilot Design Techniques about?

This document summarizes missile longitudinal autopilot designs from an optimal control perspective. A two-loop controller results from optimizing acceleration error and fin deflection, while a three-loop controller optimizes acceleration error and fin rates. A "neoclassic" four-loop controller is introduced that uses the same inputs/outputs as three-loop designs but with four gains. Higher-order designs are also discussed. The document uses a missile longitudinal dynamics model to illustrate the different

Author

Dpt Htegn

Language

EN