DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
AD0852229
Title:
Guidance Error Analysis and Orbit Determination Accuracies for the Apollo Vehicle,
Corporate Author:
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Report Date:
1961-10-04
Abstract:
The results of the error analysis presented shows the feasibility of the proposed Apollo vehicle. The assumed accuracy of the optical vehicle-borne tracker of 0.0003 radians would produce sufficient accuracy to accomplish the mission without aid of earth based trackers during the midcourse and lunar phases of the flight. Author
Pages:
0050
File Size:
0.00MB
