Autonomous navigation - The ARMMS concept

Details Autonomous navigation - The ARMMS concept Autonomous navigation - The ARMMS concept

Aug 1984

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984adans..54..523w&link_type=abstract

IN: Astrodynamics 1983; Proceedings of the Conference, Lake Placid, NY, August 22-25, 1983. Part 1 (A84-30526 13-13). San Diego,

Astronomy and Astrophysics

Astronomy

Airborne/Spaceborne Computers, Automatic Flight Control, Autonomous Navigation, Fault Tolerance, Onboard Data Processing, Satellite Navigation Systems, Space Navigation, Command And Control, Digital Navigation, Fail-Safe Systems, Geosynchronous Orbits, Orbit Calculation, Redundant Components, Reliability Engineering, Spacecraft Maneuvers, Synchronous Satellites, Trajectory Control

Scientific paper

A conceptual design is outlined for the navigation subsystem of the Autonomous Redundancy and Maintenance Management Subsystem (ARMMS). The principal function of this navigation subsystem is to maintain the spacecraft over a specified equatorial longitude to within + or - 3 deg. In addition, the navigation subsystem must detect and correct internal faults. It comprises elements for a navigation executive and for orbit determination, trajectory, maneuver planning, and maneuver command. Each of these elements is described. The navigation subsystem is to be used in the DSCS III spacecraft.

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