Investigation of High Frequency Oscillations in the OV102 Elevon Actuation Subsystems Using Continuous System Modeling Program Simulation

摘要

Two theories emerged as the cause of undesired oscillations at frequencies between 40 and 60 Hz in the Orbiter Vehicle inboard and outboard elevon actuation subsystems during hardware testing. Both the 'hardover feedback' and 'deadspace' theories were examined using continuous system modeling program simulation. Results did not support the 'hardover feedback' theory but showed that deadspace in the torque feedback spring connections to the servospools must be considered to be a possible cause of the oscillations. Further investigation is recommended.