LauncherCopter - design and development of CanSat landing quadcopter

This project involves the development of a CanSat deploying quadcopter. The goal of this project is to design a quadcopter which is able to fulfill the launching requirements of international CanSat competition, namely to deploy a CanSat weighing at most 600g at an altitude of 670m. In other words,...

Szczegółowa specyfikacja

Opis bibliograficzny
1. autor: Thong, Joseph Zhao Hang
Kolejni autorzy: Ling Keck Voon
Format: Final Year Project (FYP)
Język:English
Wydane: 2014
Hasła przedmiotowe:
Dostęp online:http://hdl.handle.net/10356/60480