Electro-opticsal sensors for docking of space vehicle

Abstract

Electro-optical sensors provide unique and critical functionality for space missions requiring rendezvous, docking, and berthing. In this paper orbital mechanics considerations, and the fundamental sensor performance requirements they impose, will be identified and parameterized. The analysis will take into account the highly sensitive interactions between (1) sensor requirements, ( 2 ) system performance cost functions, and ( 3 ) development cost, risk, and schedule. This paper will present a brief historical review of principles of operation, deve performance of electro-optical sensors at McDonnell Douglas (both internally and NASA funded) leading up capabilities. We will als 1 demonstrat to address specific needs. 34