Title :
Calculating zeroes of functions arising in various control system problems
Author_Institution :
Aeronutronic, Newport Beach, CA, USA
fDate :
12/1/1959 12:00:00 AM
Abstract :
The paper considers three separate special cases of functions for which the zeroes are determined graphically. First, the spring constant of a structural member is replaced by a complex number to allow for hysteresis losses during vibration. The corresponding characteristic function has non-conjugate zeroes which are useful in calculating frequency response, but have no meaning for transient response. Secondly, vibration acting along the input axis of a pendulous accelerometer causing displacement of the proof mass; an in-Phase cross vibration will cause a rectified torque. The real part of the compliance function is needed; knowing the zeroes is useful but not necessary in evaluating the integral over the frequency range by use of residues. Third, sampled-data systems have z transforms which often involve the sum of reciprocals of vectors. Finding real values of zeroes is simplified because only magnitudes need be considered; some graphical techniques can simplify the general vector problem. For each of the above problems alternate methods of calculation can be used; those presented are most apt to be of value to those engineers who are used to working with zeroes and poles. This paper will be published by the AIEE.
Keywords :
Accelerometers; Control systems; Data systems; Frequency response; Hysteresis motors; Springs; Torque; Transient response;
Journal_Title :
Automatic Control, IRE Transactions on
DOI :
10.1109/TAC.1959.1104872