Speaker
Description
This presentation provides an overview of the GNC subsystem of DLR’s Reusability Flight Experiment. It describes the system architecture, system design, and avionics. It focuses on the two main elements: The Guidance and Control (G&C) subsystem, which includes the functions for guidance, control, control allocation and management of the actuation systems; and the Hybrid Navigation System (HNS), which is responsible for estimating position, velocity, attitude, angular rates, and other parameters of the flight state. The requirements and boundary conditions set by the mission, the current design baseline for both subsystems, and some details about the guidance, navigation and control functions are described and discussed