introduced in this paper. The system allows the user to measure in-flight parameters such as
the arrow's speed, kinetic energy and momentum, arrow drag and vibrations of the arrow
shaft. The system consists of electronics, namely a three axis accelerometer, shock switch,
microcontroller and EEPROM memory embedded in the arrow tip. The system also includes
a docking station for download and processing of in-flight ballistic data from the tip to provide …