Flight attitude verification deviation compensation method based on flight verification

The invention discloses a flight attitude verification deviation compensation method based on flight verification, and belongs to the technical field of airborne radio navigation flight verification. The compensation method specifically comprises the following steps of 1, firstly, obtaining the coor...

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Bibliographische Detailangaben
Hauptverfasser:	WANG CHUANGANG, ZANG CHUANLEI, LIU YUNFEI, HUANG ZIGE, SHU YIHAO, XIE HONGSEN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	ANALOGOUS ARRANGEMENTS USING OTHER WAVES DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION TESTING
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Beschreibung
Zusammenfassung:	The invention discloses a flight attitude verification deviation compensation method based on flight verification, and belongs to the technical field of airborne radio navigation flight verification. The compensation method specifically comprises the following steps of 1, firstly, obtaining the coordinates of a verification type sensor antenna in a verification aircraft carrier coordinate system; 2, converting the coordinates of the verification type sensor antenna in the verification aircraft carrier coordinate system into the coordinates of the verification type sensor antenna in an airborne horizon system; 3, converting the coordinates of the verification type sensor antenna in the airborne horizon system into the coordinates of the verification type sensor antenna in a geocentric system; 4, according to the aircraft attitude information provided by a flight control system, introducing the aircraft attitude information into the coordinates of the verification type sensor antenna in the geocentric system in