This 1962 instruction manual has been ready as considered one of a sequence at the layout of ballistic missiles. It offers the equations of movement as utilized to either easy and complicated trajectory stipulations; analyzes the ability section, vacuum part, and re-entry section of missile trajectories together with some of the corrections which has to be thought of; and discusses convinced specified issues equivalent to bypass and waft trajectories, and Coriolis impression. Simplified graphs of required release angles to acquire wanted trajectories from quite a few preliminary latitudes and velocities also are integrated.
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The force, represented by a vector, has a component called the drag. This drag acts parallel to the flight direction but in the opposite sense. ” The velocity of this uniform, relative flow is called the free-stream velocity, and is represented by a vector equal and opposite to the flightvelocity vector of the body. When the body disturbs the uniform free-stream, the aerodynamic force is produced. In these terms, the drag component is parallel to the freestream velocity vector and in the same direction.
0 OI Q? Initial Misalignment of Gyros 90 160 Gyro Drift Computer Total (according to rule for addition of sigmas) Note 1. Errors for 1500 n mi missile are upper numbers in box Errors for 5500 n mi missile are lower numbers in box Note 2. (C) Platform Error. Even though the guidance system may give a missile the correct position and velocity vector with respect to the launching platform, there may be an error at impact because the platform was not in the correct geographical position and angular alignment.
C) Combined Velocity and Position Errors at Cutoff. If the probable errors in velocity and position a t cutoff are known or assumed, the probable errors in range and deflection can be estimated. For example, the range probable error is the root-meansquare of the probable error due to velocity and the probable error due to position. If the range and deflection probable errors are approximately equal, they may be replaced by the circular probable error, CEP. The CEP is the radius of the cirle that contains 50% of the impact points and has its center at the center of impact.
Ordnance Engineering Design Handbook - Ballistic Missile Series - Trajectories (U)