NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
System Finds Horizontal Location of Center of GravityAn instrumentation system rapidly and repeatedly determines the horizontal location of the center of gravity of a laboratory vehicle that slides horizontally on three air bearings (see Figure 1). Typically, knowledge of the horizontal center-of-mass location of such a vehicle is needed in order to balance the vehicle properly for an experiment and/or to assess the dynamic behavior of the vehicle. The system includes a load cell above each air bearing, electronic circuits that generate digital readings of the weight on each load cell, and a computer equipped with software that processes the readings. The total weight and, hence, the mass of the vehicle are computed from the sum of the load-cell weight readings. Then the horizontal position of the center of gravity is calculated straightforwardly as the weighted sum of the known position vectors of the air bearings, the contribution of each bearing being proportional to the weight on that bearing. In the initial application for which this system was devised, the center- of-mass calculation is particularly simple because the air bearings are located at corners of an equilateral triangle. However, the system is not restricted to this simple geometry. The system acquires and processes weight readings at a rate of 800 Hz for each load cell. The total weight and the horizontal location of the center of gravity are updated at a rate of 800/3 approx. equals 267 Hz. In a typical application, a technician would use the center-of-mass output of this instrumentation system as a guide to the manual placement of small weights on the vehicle to shift the center of gravity to a desired horizontal position. Usually, the desired horizontal position is that of the geometric center. Alternatively, this instrumentation system could be used to provide position feedback for a control system that would cause weights to be shifted automatically (see Figure 2) in an effort to keep the center of gravity at the geometric center.
Document ID
20100014097
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Johnston, Albert S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Howard, Richard T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Brewster, Linda L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2006
Publication Information
Publication: NASA Tech Briefs, January 2006
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-31999-1
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available