System and method for determining the attitude of a space vehicle
阅读：181发布：2023-07-15
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1. THE METHOD OF DETERMINING THE ATTITUDE OF A SPACE VEHICE WITH REFERENCE TO A FIRST LINE EXTENDING VERTICALLY FROM THE CENTER OF A PLANET TO THE VEHICLE COMPRISING THE STEPS OF; SCANNING THE PLANET FROM SAID VEHICLE IN TWO MUTUALLY PERPENDICULAR PLANES; AND FOR EACH SCAN DETERMINING THE TIME INTERVAL BETWEEN THE INSTANT WHEN HALF OF A PLANET SCAN HAS OCCURRED AND THE INSTANT WHEN THE SCAN COINCIDES WITH THE LINE DEFINED BY THE INTERSECTION OF THE SCANNING PLANES.
21. A SYSTEM FOR DETERMINING THE ATTITUDE OF A SPACE VEHICLE WITH REFERENCE TO A FIRST LINE EXTENDING VERTICALLY FROM THE CENTER OF A PLANET TO THE VEHICLE COMPRISING: FIRST AND SECOND SCANNING MEANS IN SAID VEHICLE FOR GENERATING TWO NARROW SEARCH BEAMS AND FOR SIMULTANEOUSLY CONTINUOUSLY ROTATING THE SAME WITH CONSTANT ANGULAR VELOCITY IN TWO MUTUALLY PERPENDICULAR PLANES; AND A PAIR OF COMPUTING MEAN RESPECTIVELY COUPLED TO SAID SCANNING MEANS FOR COMPUTING THE ANGLE THROUGH WHICH EACH BEAM MOVES BETWEEN A LINE MIDWAY BETWEEN ITS POINT OF INITIAL INTERCEPTION OF THE PLANET AND ITS POINT OF FINAL DEPARTURE FROM THE THE PLANET AND A SECOND LINE DEFINED BY THE INTERSECTION OF SAID PLANES; EACH OF SAID COMPUTING MEANS COMPRISING MEANS RESPONSIVE TO THE RESPECTIVE BEAM FOR GENERATING A STEPPED SIGNAL HAVING A WIDTH PROPROTIONAL TO THE BEAM INTERCEPTING PLANET, MEANS COUPLED TO THE RESPECTIVE SCANNING MEANS FOR PROVIDING
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