Our objective is to develop a guidance module
that adds reactive guidance to an existing missile system.

This will include:

Programming microprocessor to control system

Incorporating GPS and IMU systems

Simulating external and internal forces on model

Building functional model

Documentation Information:

Source Code

Altera Nios Cyclone II Development Kit
Altera Cyclone FPGA Family Data Sheet
Honeywell Gunhard IMU
Servomotor Information
NACA Designations


MK66 final report