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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1990, Vol. 11 ›› Issue (5): 288-293.
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Shen Gongxun, Zhou Zhiming
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Abstract: In this paper, the maneuver ballistic missile parametric correction in the burning phase with star light is studied, when the maneuver ballistic missile is launched under the condition that the initial position is not exactly defined and the inertial navigation platform is not completely leveled and aligned.
Key words: star sensor, star light, star map
Shen Gongxun;Zhou Zhiming. MANEUVER BALLISTIC MISSILE CORRECTION IN THE BURNING PHASE WITH STAR LIGHT[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(5): 288-293.
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https://hkxb.buaa.edu.cn/EN/Y1990/V11/I5/288