초록 ▼

The life of a target satellite is modified, i.e., extended or terminated by docking an extension spacecraft with the target satellite to form a docked satellite-spacecraft combination. The extension spacecraft is docked with and mechanically connected to the target satellite and includes guidance, n

The life of a target satellite is modified, i.e., extended or terminated by docking an extension spacecraft with the target satellite to form a docked satellite-spacecraft combination. The extension spacecraft is docked with and mechanically connected to the target satellite and includes guidance, navigation, and control systems for performing the rendezvous and docking maneuvers and for controlling the position of the docked spacecraft-satellite combination. The extension spacecraft also includes an onboard propellant supply for accomplishing the rendezvous and docking of the spacecraft with the satellite and for controlling the position of the docked spacecraft-satellite combination. A remote cockpit system is provided to permit human control of the extension spacecraft during proximity operations.

대표청구항 ▼

[ Having described by invention in such terms as to enable those skilled in the art to understand and practice it, and having identified the presently preferred embodiments thereof, I claim:] [1.] A ground control remote cockpit system for remotely controlling operations of an orbitable spacecraft c

[ Having described by invention in such terms as to enable those skilled in the art to understand and practice it, and having identified the presently preferred embodiments thereof, I claim:] [1.] A ground control remote cockpit system for remotely controlling operations of an orbitable spacecraft comprising:a cockpit system situated at a location remote from said spacecraft, said cockpit further including;(a) a guidance, navigation and control computer for said spacecraft, located in said cockpit remote from said spacecraft;(b) a spacecraft variables display system located in said remote cockpit, including a visual display for displaying signals down-linked through said computer from television camera means and motion sensor means onboard said spacecraft; and(c) control means adapted to be manually operated by a human pilot in said remote cockpit in response to displays on said display system, said control means including means to generate pilot input signals through said computer which provide control of attitude and velocity of said spacecraft, said pilot input signals up-linked to said spacecraft to control sad spacecraft during operations of said spacecraft.