06.1 - Flight Dynamics and Control (Control & Modelling)
DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULE
C. Krause¹, C. Göttlicher¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, Germany
The Institute of Flight System Dynamics (TUM) is developing flight control software for OPVs and UAVs. Therefore flight tests are performed to verify flight dynamic models, identify actuator dynamics or evaluate controller performance. This paper describes the development of a software module, which is able to inject various flight test maneuvers into the controller or directly to the actuators.