Matlab implementation to simulate the non-linear dynamics of a fixed-wing unmanned areal glider. Includes tools to calculate aerodynamic coefficients using a vortex lattice method implementation, and to extract longitudinal and lateral linear systems around the trimmed gliding state.
Right now, Message/Request/Response is only implemented if there exists some Type ID. This is correct behavior for standard definitions. For other definitions, type ID can be resolved dynamically and needs to be implemented even though there's no statically defined type ID.
Some check based on if the definition is inside the uavcan namespace or not needs to be implemented.
A curated list of aerospace/space related data and code resources for a community of independent hackers dedicated to furthering humanity's knowledge of the universe through open collaboration.
This project outputs G-code that is used to control a 4-axis hot wire cutter, employed to cut a wing / airfoil from a physical block of foam. Effectively, it is a slicer for a particular arrangement of raw-coordinate data files.
Right now, Message/Request/Response is only implemented if there exists some Type ID. This is correct behavior for standard definitions. For other definitions, type ID can be resolved dynamically and needs to be implemented even though there's no statically defined type ID.
Some check based on if the definition is inside the uavcan namespace or not needs to be implemented.