Abstract

A long-range investigation into the transmission, utilization, and processing of information for missiles and space vehicles has been initiated. The ultimate objective is a theory of control and communication for such vehicles which would relate the principles of information theory to the design philosophy of the control and communication systems. In investigating such information-theoretic guidance control problems, it is necessary to consider the effects of noise, both internal and external, on any possible computation control process. The external noises would arise in communication links, the drifts of gyros, possible variations in external conditions, variations in amounts and rates of rocket burning, and other causes. The internal noises could be those electronically generated (such as shot and Johnson noises) and those generated by digital computation processes. It is desirable to begin with simple but representative problems. In the event that an incremental digital or analog computer is part of a control loop, a typical problem would be signal plus noise into an analog or digital integrator.

Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.