Ballistic trajectory optimization method capable of meeting coverage requirement of special-shaped antenna pattern
The invention discloses a trajectory optimization method capable of meeting the coverage requirement of a special-shaped antenna pattern. The trajectory optimization method comprises the steps that the position of a measuring station relative to an aircraft under a transmitting system is acquired; o...
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| creator | GUAN JIAN YUAN JIANGBO WANG SHAOHUA LI ZHENHUA XUE PENGFEI GUO HAO ZHANG JIN TIAN SHICHAO XIAO ZHEN SU HANSHENG WU XIAOHUA SONG ZHONGJU SUN SHIJIE REN LIANG XU YU |
| description | The invention discloses a trajectory optimization method capable of meeting the coverage requirement of a special-shaped antenna pattern. The trajectory optimization method comprises the steps that the position of a measuring station relative to an aircraft under a transmitting system is acquired; obtaining the position of the measuring station relative to the aircraft under the aircraft missile system according to the position of the measuring station relative to the aircraft under the launching system; obtaining the position of the measuring station in the aircraft antenna view field according to the position of the measuring station relative to the aircraft under the aircraft missile system; obtaining the measurement and control coverage of the trajectory according to the position of the measurement station in the field of view of the aircraft antenna; and with optimal measurement and control coverage as a target, ballistic optimization is completed. According to the method, the trajectory optimization des |
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The trajectory optimization method comprises the steps that the position of a measuring station relative to an aircraft under a transmitting system is acquired; obtaining the position of the measuring station relative to the aircraft under the aircraft missile system according to the position of the measuring station relative to the aircraft under the launching system; obtaining the position of the measuring station in the aircraft antenna view field according to the position of the measuring station relative to the aircraft under the aircraft missile system; obtaining the measurement and control coverage of the trajectory according to the position of the measurement station in the field of view of the aircraft antenna; and with optimal measurement and control coverage as a target, ballistic optimization is completed. 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The trajectory optimization method comprises the steps that the position of a measuring station relative to an aircraft under a transmitting system is acquired; obtaining the position of the measuring station relative to the aircraft under the aircraft missile system according to the position of the measuring station relative to the aircraft under the launching system; obtaining the position of the measuring station in the aircraft antenna view field according to the position of the measuring station relative to the aircraft under the aircraft missile system; obtaining the measurement and control coverage of the trajectory according to the position of the measurement station in the field of view of the aircraft antenna; and with optimal measurement and control coverage as a target, ballistic optimization is completed. 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The trajectory optimization method comprises the steps that the position of a measuring station relative to an aircraft under a transmitting system is acquired; obtaining the position of the measuring station relative to the aircraft under the aircraft missile system according to the position of the measuring station relative to the aircraft under the launching system; obtaining the position of the measuring station in the aircraft antenna view field according to the position of the measuring station relative to the aircraft under the aircraft missile system; obtaining the measurement and control coverage of the trajectory according to the position of the measurement station in the field of view of the aircraft antenna; and with optimal measurement and control coverage as a target, ballistic optimization is completed. According to the method, the trajectory optimization des</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS |
| title | Ballistic trajectory optimization method capable of meeting coverage requirement of special-shaped antenna pattern |
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