Accession Number:

AD0607714

Title:

GUIDANCE SCHEMES FOR ROCKET VEHICLES

Descriptive Note:

Corporate Author:

TRW SPACE TECHNOLOGY LABS LOS ANGELES CA

Personal Author(s):

• Sarture, C. W.

Report Date:

1960-10-13

Pagination or Media Count:

62.0

Abstract:

Inertial guidance for rocket vehicles is discussed. The material is concerned mainly with the proper utilization of inertially derived position and velocity data in a way which will fulfill the mission objectives.

Descriptors:

• *GUIDED MISSILES
• *INERTIAL GUIDANCE
• VELOCITY
• GUIDED MISSILE TRAJECTORIES
• FLIGHT CONTROL SYSTEMS
• INSTRUMENTATION
• GEOMETRY
• MATHEMATICS
• GUIDANCE
• EQUATIONS

Subject Categories:

• Guided Missile Trajectories, Accuracy and Ballistics
• Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE