Research Article

Variable-Time-Domain Online Neighboring Optimal Trajectory Modification for Hypersonic Interceptors

Table 1

The related parameters of booster engine.

Parameter nameValue

(stage 1/2)280/200 (s)
(stage 1/2)30/8.9 (kg/s)
Burning time (stage 1/2)20/50 (s)
Mass of booster shell250 kg
Mass of interceptor60 kg