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

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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

Author(s):
Munro, G. C.
Author Organization(s):
JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Pagination:
0005

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
CM-137
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application
Communities of Interest:
Weapons Technologies
Descriptor(s):
(*GUIDANCE, EQUATIONS), BEAM RIDER TRAJECTORIES, GUIDED MISSILE TRAJECTORIES, GUIDED MISSILES, ACCURACY, EQUATIONS OF MOTION, STABILITY
Field(s)/Group(s):
Guided Missile Trajectories, Accuracy and Ballistics
Report Date:
1945 Oct 29