Online prediction guidance method for glider interception near hypersonic target and electronic equipment

The invention discloses a near hypersonic target glider motion interception online prediction guidance method and electronic equipment, and the method comprises the steps: 1, simplifying a non-cooperative near hypersonic target into an equal-height uniform-speed level flight or equal-height uniform-...

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Bibliographische Detailangaben
Hauptverfasser: LU YING, MENG WENXIA, ZHANG CHENHAN, LI HAOYUE, LI LUOGANG, BAO NUO, YAN YAN, CHAO LUJING, CUI BIYING, WANG ZHENYA, REN JINLEI, ZHANG JIA, LI SHANSHAN
Format: Patent
Sprache:chi ; eng
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Zusammenfassung:The invention discloses a near hypersonic target glider motion interception online prediction guidance method and electronic equipment, and the method comprises the steps: 1, simplifying a non-cooperative near hypersonic target into an equal-height uniform-speed level flight or equal-height uniform-speed-reduction level flight analysis track according to a power form; 2, on the basis of a target analysis prediction trajectory, selecting a prediction interception point on line, and taking the projection speed and relative distance information of a sub-satellite point of an interception aircraft as main analysis parameters; 3, on the basis of a predicted interception point selection result and the instantaneous resistance overload demand calculated at the same time, calculating a flight attack angle sequence of the interception aircraft on line according to a rendezvous aircraft aerodynamic parameter database and a difference value; and 4, according to the predicted interception point, selecting a flight direct