Method and apparatus for iterated determinations of sensed speed and speed governing

• US 5,222,022 A
• Filed: 12/06/1990
• Issued: 06/22/1993
• Est. Priority Date: 12/01/1986
• Status: Expired due to Term

• Current Assignee: Woodward Governor Company
• Original Assignee: Woodward Governor Company
• Inventors: Adams, Larry L., Garvey, Daniel C.
• Primary Examiner(s): Trans, Vincent N.
• Application Number:
  US07/624,492
• Time in Patent Office: 929 Days
• Field of Search: 364/431.07, 364/431.04, 364/565, 123/414, 123/416, 123/417, 123/418, 123/419
• US Class Current: 701/110
• CPC Class Codes: F02D 2041/1409 using at least a proportional, integral or derivative controller
• CPC Class Codes: F02D 2041/1422 Variable gain or coefficients
• CPC Class Codes: F02D 2041/288 for performing a transformation into the frequency domain, e.g. Fourier transformation
• CPC Class Codes: F02D 2200/1015 Engines misfires
• CPC Class Codes: F02D 31/007 controlling fuel supply
• CPC Class Codes: F02D 41/0097 using means for generating speed signals
• CPC Class Codes: F02D 41/1498 measuring engine roughness
• CPC Class Codes: G01P 3/489 Digital circuits therefor

Abstract

Methods and apparatus, preferably carried out with the aid of a programmed digital computer for iteratively determining the actual speed of an engine and iteratively updating a fuel rate command signal so as to govern and correctively remove any errors from the set point speed. Jumps to a program subroutine are triggered by sensing the engine crankshaft to generate a predetermined number Q of pulses during the span of one revolution (where Q is an integer greater than 1), and each pass through the subroutine determines the actual engine speed as an average over the last whole revolution of the crankshaft. There are thus Q iterations per revolution but each interation signals the speed over one whole revolution. This results in wholly eliminating torsionally induced speed fluctuations, or the like, from the determined speed signal. Each pass through the program subroutine also determines the speed error and updates the fuel rate command signal as a PID function of such error. Because this iterated updating occurs, not at a regularly timed rate, but at intervals which vary inversely with speed, the instructions of the subroutine program can be made very short and simple while nevertheless causing effective automatic tuning adjustments of the integral gain, stability and compensation factors.

Claims

1. A method for controlling a desired rotational speed (S_d) of a rotating shaft of an engine driving a variable load, the rotating shaft having a plurality of markers circumferentially distributed about the shaft, the method comprising the steps of:

determining time periods (T) for whole revolutions of each of the markers past a reference point;

determining an average time period for the determined time periods (T);

deriving an operating speed (S) of the rotating shaft based on the averaged time period;

generating a value of a common signal (F) for each of the markers from a proportional-integral-derivative (PID) function related to an error between the desired speed (S_d) of said shaft and the operating speed (S) of the shaft,

wherein the PID function is defined according to the relation;

##EQU23## controlling the speed of the shaft in response to the value of the command signal (F); and

updating the command signal (F) for every whole revolution of each of the markers.

2. The method as set forth in claim 1 where:

z^-1 represents a mathematical operator;

I_R is a predetermined constant representing an integral gain factor;

each T_R is a predetermined constant representing a time period for a whole rotation of a marker at a top speed or a variable inversely proportional to the operating speed;

each S_R is a predetermined constant representing the top speed of the rotating shaft or a variable representing the operating speed (S);

F_i-1 is a previous value of the command signal (F), which is substantially proportional to the torque of the load;

F_max is a predetermined constant representing a maximum value of the command signal (F);

B_R is a predetermined constant representing a stability factor; and

D_R is a predetermined constant representing a compensation factor.