
6/29/2017
What this post added
This post details the successful second full-scale test flight of the Aquila aircraft, focusing on the technical modifications and data gathered. Key engineering contributions include the addition of 'spoilers' for landing control, integration of hundreds of sensors (strain gauges, IMUs) for structural and aerodynamic data collection, modifications to autopilot software, and improvements to the communication subsystem. The flight successfully gathered data on drag through 'trim shots' and verified the performance of new components, leading to a climb rate nearly twice that of the first flight. The landing mechanism, utilizing Kevlar pads and propeller stopping, was also tested, with one propeller failing to lock horizontally as intended. The data collected will be used to refine aerodynamic and structural models for optimizing battery and solar array size.