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Design of a Thruster Vector Servo-Elastic FilterThis presents a method to improve the thruster vector servo elasticity (TVSE) stability. TVSE is the coupling between the TVC system engine dynamics and the vehicle flexible modes. It can lead to instability of the flexible modes due to the energy injection from the thrust. For large boosters with heavy TVC engine, TVSE is more likely to cause instability. This instability is part of the plant dynamics and is not detected by the flight control. In this paper, the TVSE is treated as a disturbance rejection problem with the inertial force of the flexible motion viewed as an external disturbance to the TVC actuator control system. By effectively rejecting this disturbance, the engine can be decoupled from the flexible dynamics thus improving TVSE stability. The actuator disturbance transfer function is modified by inserting a TVSE filter into the control system. The filter aims to reduce the magnitude and introduce phase lead of the disturbance transfer function over the TVSE sensitive frequency range while maintaining adequate stability margins of the actuator control system. A prefilter is also designed for good command tracking. The filter and prefilter resulting from this method are usually of low order and can be included to the existing actuator controller if the controller is programmable. This method was demonstrated for a hydraulic Simplex actuator model. Its applications to SLS B1 and B2 TVC actuator are also described. B2 actuator controller is modified based on this method. The tradeoff between TVSE stability and the control system stability can be balanced by adjusting the amount of phase lead introduced by the TVSE filter. This method provides a useful way to solve the TVSE instability issue without costly and time-consuming a TVC system redesign. This method is based on the basic control principles of loop shaping and disturbance rejection and has been proven to be effective under proper circum-stances.
Document ID
20240016089
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Wei Wu
(Amentum Chantilly, Virginia, United States)
Date Acquired
December 16, 2024
Subject Category
Spacecraft Propulsion and Power
Aerodynamics
Meeting Information
Meeting: 35th AAS/AIAA Space Flight Mechanics Meeting
Location: Kaua'i, HI
Country: US
Start Date: January 19, 2025
End Date: January 23, 2025
Sponsors: American Institute of Aeronautics and Astronautics, American Astronautical Society (AAS)
Funding Number(s)
CONTRACT_GRANT: 80MSFC18C0011
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Thrust vector control
thrust vector servo elasticity
disturbance rejection
phase lead
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