Accession Number:

AD0659105

Title:

GUIDANCE EQUATIONS. SIMPLE PITCH (YAW) CONTROL CONSIDERING RADAR DELAY, ERROR SIGNAL AND SERVO RESPONSE,

Descriptive Note:

Corporate Author:

JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB

Personal Author(s):

Report Date:

1945-10-29

Pagination or Media Count:

5.0

Abstract:

The equations which describe with a fair degree of accuracy the performance of a missile being guided along a beam are written. No attempt is made to solve the equations it is suggested that they be solved by a differential analyzer, should one become available, in order 1 to determine whether or not the system represented by the equations is stable and 2, if the system is stable, to obtain as nearly as possible optimum values of the parameters involved. Author

Subject Categories:

  • Guided Missile Trajectories, Accuracy and Ballistics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE