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Robust Control Algorithm for a Two Cart System and an Inverted PendulumThe Rectilinear Control System can be used to simulate a launch vehicle during liftoff. Several control schemes have been developed that can control different dynamic models of the rectilinear plant. A robust control algorithm was developed that can control a pendulum to maintain an inverted position. A fluid slosh tank will be attached to the pendulum in order to test robustness in the presence of unknown slosh characteristics. The rectilinear plant consists of a DC motor and three carts mounted in series. Each cart s weight can be adjusted with brass masses and the carts can be coupled with springs. The pendulum is mounted on the first cart and an adjustable air damper can be attached to the third cart if desired. Each cart and the pendulum have a quadrature encoder to determine position. Full state feedback was implemented in order to develop the control algorithm along with a state estimator to determine the velocity states of the system. A MATLAB program was used to convert the state space matrices from continuous time to discrete time. This program also used a desired phase margin and damping ratio to determine the feedback gain matrix that would be used in the LabVIEW program. This experiment will allow engineers to gain a better understanding of liquid propellant slosh dynamics, therefore enabling them to develop more robust control algorithms for launch vehicle systems
Document ID
20110015819
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
Wilson, Chris L.
(Mississippi State Univ. Mississippi State, MS, United States)
Capo-Lugo, Pedro
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M11-0979
Report Number: M11-0979
Distribution Limits
Public
Copyright
Public Use Permitted.
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