Position control system of the discontinuous feedback type
AssigneeThe Boeing Company
InventorPatrick J. Hawkins
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AssigneeThe Boeing Company
InventorPatrick J. Hawkins
Estimating the term…
A position control system is disclosed for aiming a mobile rocket launcher having positionable axes in the azimuth and elevation planes. The control system has a separate control subsystem for each axis of movement, and each such subsystem includes an initial aiming signal processor providing a course positioning function and a reaiming signal processor providing a fine positioning function. The initial aiming processor receives signals representing a desired position (DP), a feedback signal representing the actual position (AP) updated at predetermined sampling intervals, and an error signal (E) representing the difference between DP and AP. From signals representing AP and E, and a constant representing the stopping time of the launcher mechanism for a given control axis, the initial aiming processor produces a predicted position signal (PP) which represents the position that the launcher will reach upon termination of the actuator drive for that axis. The signal PP is then compared with the signal representing DP and depending upon a predetermined relationship between the predicted and desired positions of the launcher an actuator control signal is generated for driving the associated actuator at either a full forward or full reverse speed, or stopping and braking the associated launcher mechanism. The reaiming processor incorporates an error averaging network and an actuator signal function generator. The former averages, over a given time interval, the magnitude and directon of the error signal E, and the latter is responsive to the time average error (AE) to generate a forward or reverse actuator drive signal for an incrementally variable duration T.sub.c, that increase or decrease with the magnitude of AE and is timed to remove any remaining error in the position of the launcher for the given control axis. The reaiming processor is reactivated after each rocket launching to reaim the launcher to correct for any disturbance to its original position caused by the firing recoil, and the correlation provided by the function generator between the average error AE and the signal duration T.sub.c is updated from time to time to compensate for varying actuator drive characteristics due to wear and environmental conditions.
A control apparatus for positioning a dynamically controlled mechanism having at least a first axis of controlled movement, comprising in combination:
In a control apparatus for positioning a dynamically controlled unit that has at least a first axis of controlled movement and including actuator means operatively associated with said controlled unit and having forward and reverse drive modes for displacing said unit with respect to said given axis and having a stop mode, and means for producing an error signal (E) representing the difference between a desired and an actual position of said controlled unit, wherein the improvement comprises a signal processor connected to receive said error signal E for responsively producing an actuator drive signal for selectively disposing said actuator means in one of said modes, and wherein said signal processor comprises a signal averaging means for taking a time average of said error signal E for a predetermined time interval to develop a discrete time averaged error signal (AE);
A control apparatus for positioning a dynamically controlled unit having at least a first axis of controlled movement, comprising in combination:
A method of controlling the position of a dynamically controlled mechanism wherein a mechanism actuator is selectively operated in forward or reverse drive modes or a stopped mode by an actuator drive signal developed in response to signals representing desired position (DP), actual position (AP) and a position error (E) which is the difference between signals DP and AP, comprising the steps of:
In a method of positioning a dynamically controlled unit that has at least a first axis of controlled movement and includes operating an actuator for displacing said controlled unit in forward and reverse drive modes, and for stopping said unit when in a stop mode, and wherein an error signal (E) is produced for representing a difference between a desired position (DP) and an actual position (AP) of said controlled unit, the improvement in said method comprising the steps of:
Dependencies are inferred from the claim text.