Summary: Short-Take-Off and Landing (STOL) aircraft are used in commercial and military industry. They reduce the necessary runway needed, therefore increasing the flow of airport traffic, increase accessibility of smaller airports, and reduce noise pollution due to faster rates of climb and decent. These favorable aspects come at cost of increase fuel burn limiting range, speed, payload, and stability of the aircraft. At the same time, unmanned aerial vehicles (UAVs) are a becoming common place. Due to the control software of UAVs it is possible to program take-offs and landings. Short take-off can be optimized through a UAV platform replicating a scale private aircraft with several short-take-off and landing functions.
Objective: Optimize an aircraft for short-take-off and landing capabilities of an existing UAV platform.
System: Consists of an unmanned Sig-70 low-scale aircraft modified to house an Ardupilot Autopilot and GPS (Figure 1 & 2), Short-Take-Off and Landing Devices (Figure 3), and a fast prototyping system using MATLAB/Simulink, Real-Time C++ Complier, and ERAU Support Block set to transmit and receive flight data to the Ardupilot autopilot (Figure 4).
Contributions:
(August 2013 - May 2014)
Summary: The objective of the competition is to build and launch a hybrid powered rocket. There are two categories of competition to choose from. The first category consists of launching a hybrid rocket to the maximum altitude. The second category challenges the teams to fly their rocket closest to 2000 feet in altitude. There must be at least two teams competing in each category. If there is only one team, that team will be asked to move to the other category. - Flordia Space Grant
Contributions:
(August 2013 - May 2014)
(October 2011 - April 2012)