Russia launched two multistage ballistic missiles in 1960. The deviation of the landing point with respect to trajectory range was only one sixth-thousandth and the deviation of speed of flight was three-one-hundred-thousandths, which indicated that a condition of high perfection had been reached in rocket control systems. The operating principles of rocket control systems were introduced. The function of rocket control systems was explained. A block diagram and three major components of the automatic stabilizer were discussed. These components are: position fixing element; amplification/conversion device and steering mechanism. Finally, speed measurement mechanisms were brought up since target accuracy is greatly influenced by errors in speed. What the author introduced was simply a concept of control system equipment. (Author)
Discussion of the Control Systems of Ballistic Rockets
1970
9 pages
Report
No indication
English
Impact points of ballistic rockets
Engineering Index Backfile | 1957
|Method for calculating impact points of ballistic rockets
Engineering Index Backfile | 1957
|A Problem of Optimum Motion of Ballistic Rockets
NTIS | 1966
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