NAVAL ORDNANCE AND GUNNERY
VOLUME 2, FIRE CONTROL

CHAPTER 26
RELATIVE-RATE ANTIAIRCRAFT SYSTEMS
HOME          INDEX
Chapter 26 Relative-rate Antiaircraft Systems
A. Fire Control Problem

B. Basic elements of lead-computing sights
C. Gun sight Mark 15
D. Gun Fire Control System Mark 63
E. Gun Fire Control System Mark 56
                                                C. Gun Sight Mark 15

26C1. Introduction

Gun Sight Mark 15 is an example of a gyroscopic lead-computing sight which is designed for the control of heavy machine guns and dual-purpose guns at short and intermediate ranges. It may be used against targets with range rates up to 350 knots (800 knots in some modifications) and at ranges up to a maximum of 7,500 yards. In addition to its use as a complete fire control system in itself, Gun Sight Mark 15 is used in some modifications of the Gun Fire Control System Mark 63, which will be described later in this chapter.

26C2. Physical description
Figure 26C2 shows a mechanical schematic representation of the Mark 15 sight. The entire mechanism shown in this figure is enclosed in a case, which is shown in figure 26C1. In addition to the mechanism contained in the sight case, several other items of equipment are required. These items include:

1. A supporting platform which provides the freedom of movement in train and elevation necessary for tracking targets.

2. A unit to supply compressed air to drive the gyros.

3. A unit to solve the geometry of wind ballistic corrections.

4. A mechanical means of introducing range and range rate values.
The Mark 15 sight may be mounted on any of several types of supporting platforms. For use as a simple fire control system it is mounted on a Gun Director Mark 51. Such a director is shown in figure 26C3, equipped with a short-range lead-computing sight, the Mark 14, which is somewhat simpler than the Mark 15. For use as a part of a more elaborate system, the sight may be installed on a Mark 52 director, as shown in figure 26C1, or on a Mark 1 director pedestal, as shown schematically in figure 26D1.
An air supply unit is furnished with each sight and installed near the sight. This unit provides a supply of dried, compressed air at a constant pressure to the sight for spinning the rate-of-turn gyros.  Wind rates are transmitted to the sight as a-c electrical potentials by Wind Transmitter Mark 4. This unit receives inputs of own ship’s course and speed, true wind direction and speed, and gun train order, and resolves them into traverse wind rate and horizontal range wind rate. These wind rates are sent as electrical inputs to torque motors secured to the output shafts of the train and elevation gyros.

The method of introducing range and range rate into the gun sight varies in different installations. In the simplest arrangement only a knob is provided for each of these inputs. In most cases, however, some type of range receiver is provided. Some of these receivers provide only for matching dials or zero readers manually to introduce range and range rate. Others provide for automatic range input and manual range rate input, while even more elaborate range receivers provide automatic inputs of both range and range rate as received from an associated radar.
26C3. Functional description

Gun Sight Mark 15 utilizes two rate-of-turn gyros, one for train (traverse) lead angle and one for elevation lead angle. The gyros are air-driven, and rotate at approximately 8,300 revolutions per minute. Air to drive the gyros comes from an air supply unit associated with the sight, and in order to maintain a constant speed of rotation of the gyro, the air is kept at a constant temperature and pressure. Each gyro rotor is mounted in a gimbal frame which is in turn mounted in the gyro case by a frictionless suspension. The gyro rotors are oriented with their spin axes perpendicular to the fore-and-aft axis of the sight case and to each other, so that the train gyro responds only to motion in the traverse plane and the elevation gyro responds only to motion in the elevation plane. Each gyro’s output shaft is restrained by a range spring at one end, while on the other end a torque motor is mounted to provide for the introduction of wind ballistic corrections. On the same end as the torque motor are one or more weights for the purpose of making ballistic corrections for drift and superelevation.

Figure 26C4
illustrates the action of the super-elevation weight on the elevation gyro. The force of gravity acting on the weight causes a rotation of the gyro output shaft against the restraint of the range spring. Since the range spring is weaker at long ranges, the correction applied at these ranges is greater. Since present range is the range input to the sight, and superelevation should be calculated on the basis of advance range, a variable superelevation weight is provided which can be adjusted to give a larger or smaller correction, depending upon the range rate input. This may be seen in figure 26C2. The effect of the gun elevation on the superelevation weight may be seen from figure 26C4. It will be noted that a superelevation weight is mounted on the train gyro also. The reason for this weight is that superelevation must be corrected in the vertical plane, and if trunnion tilt is present, a vertical correction requires two components: one in train and one in elevation. Thus the effect of trunnion tilt is eliminated. A drift weight is also provided on the output shaft of the train gyro. Its action is similar to that of the superelevation weight on the elevation gyro, with the exception that no correction is made for range rate.

At each end of the gyro case is a damper assembly, consisting of a disc attached to the output shaft of the gyro, and a housing secured to the case. The damper housing is partially filled with a damping fluid in which the disc rotates. The purpose of the damper assembly is to smooth out the response of the gyro during tracking. This makes tracking easier and helps prevent the generation of false lead angles as a result of tracking errors. The damping fluid applies a restraining torque to the output shaft which varies with the rate of change of the lead angle. In steady tracking the lead angle is not changing, in which case the fluid has no restraining effect. Therefore the magnitude of the lead angle is not affected. The damping fluid is very viscous when cold, and its viscosity varies greatly with changes in temperature. In order to prevent changes in the ambient temperature from changing the viscosity of the fluid, and therefore the damping characteristics, internal heaters are used to stabilize the temperature at a value higher than any ambient temperature likely to be encountered.
The optical system of Gun Sight Mark 15 includes a telescope, lead angle mirrors, spot mirrors, an optical filter, a reticle plate, and reticle illumination. In addition, some modifications include a cathode-ray tube and a pellicle for introducing its image into the line of sight. The arrangement of the optical system is shown in figure 26C5. The target image, after entering the sight case, is reflected from the elevation lead angle mirror to the traverse lead angle mirror, thence through the telescope objective lens to the deflection spot mirror. From here it is reflected to the elevation spot mirror, and then through the reticle plate to the telescope eyepiece assembly. When either of the gyros precesses, it actuates a linkage to offset the corresponding lead angle mirror, thus deflecting the target image. Since the position of the reticle is fixed, this means that the target image will no longer be centered in the reticle. The sight case must then be moved so as to bring the target image back into the reticle circle. The arrangement of the mirrors is such that the sight case must be offset ahead of the target in order to center the image. This causes the sight case axis to lead the target by the necessary amount of lead angle. In a similar manner, the introduction of spots deflects the target image and necessitates a change in the lead angle.

In those modifications of the sight which incorporate provisions for radar tracking, a cathode-ray tube is installed in the sight case. The radar image is reflected from a mirror to a pellicle in the optical axis of the telescope. This pellicle is a very thin plastic sheet which is semi-transparent, so that it reflects the radar image through the reticle plate to the telescope eye-piece, but still allows the optical target image to pass through for optical tracking. In radar tracking, the optical target image is blocked out by increasing the density of the optical filter; the intensity is turned up on the radar scope; and the radar image, (a bright spot) is kept centered in the reticle.

When the Mark 15 sight is used in conjunction with a radar, the radar antenna must be caused to lag the motion of the gun bore, in order to remain on target when the gun is offset by the computed lead angle. This is accomplished by providing a separate power drive for the antenna. Electrical signals originating in the gyro pick-off transformers and defining the magnitude and direction of the lead angles are used to control the antenna power drive. In some cases, the radar antenna is mounted on the director, while in other cases it is located on the gun mount. The electrical signals from the pick-off transformers actuate the radar antenna power drive to offset the antenna by the amount of the computed lead angle, but in the opposite direction from the target’s motion. In bringing the antenna back on target, by centering the target image in the reticle, the sight case and the gun bore are offset ahead of the line of sight by the proper lead angles. Thus, when the radar target image is centered in the reticle circle, the gun will be properly positioned to fire at the target.

26C4. Operation

In preparing Gun Sight Mark 15 for operation, the unit must first be warmed up. The warming-up process requires a period of about 30 minutes for bringing the damping fluid to its operating temperature and viscosity. Bringing the gyros up to their designed operating speed requires about 6 minutes. When operating in an area where attack is likely, the sights are kept warmed up and ready for use.

Preliminary to firing, the target is located by means of a fixed auxiliary telescope mounted on top of the sight. The target is tracked briefly through the auxiliary telescope, after which the operator shifts to the gun-sight telescope. During this initial process the range is kept set at the minimum value in order to restrict movement of the gyro, or, if gyro cagers are installed, the gyros are kept caged. When the target image has been centered in the reticle circle, the cager is released and the proper range and range rate are set in. ‘A similar process is used for radar tracking, except that in this case the auxiliary telescope cannot be used.

Tracking the target or radar spot is continued. The target or spot is kept centered in the reticle circle by smooth movement of the director. It is essential that all tracking movements be smooth, since sudden movements cause the generation of false lead angles.

During tracking, the appropriate values of range and range rate are continually set into the sight. If no radar is provided, estimated ranges must be set in. In this case the range setter should determine whether the range is set correctly by observing the projectile tracers. For an incoming target, which is the usual case, the range should be set initially so that the tracers pass just behind or below the target. Tracers passing behind the target indicate that the lead angles are too small. This is the case when the range setting is less that the actual range, as a short range setting causes the restraining springs on the gyros to be stiff. It is readily apparent that, as the target approaches, the actual range will agree more closely with the set range, and the tracer stream will move toward the target. When the actual and set ranges are equal, the tracers should be hitting the target. As the actual range becomes less than the set range, the tracers will pass ahead of the target, because the generated lead angles are too large. Now the range setting must be decreased to make the tracers again pass behind the target.

Thus the range setting procedure is as follows:

1. Set range so that tracers pass just behind or below target.

2. Wait for tracer stream to pass through target.

3. When tracers are passing ahead of target, decrease range setting and repeat steps 1 and 2.