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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.

  • Updated Feb 28, 2017
kjetilkjeka commented Nov 8, 2017

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.

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