Analytical solution method for hypersonic velocity smooth gliding trajectory under rotating earth
A gliding ballistic and hypersonic technology, applied in the field of weapons and aerospace technology, can solve problems such as difficult to meet precise guidance, analysis and correction, low accuracy, tracking error, etc.
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[0549] In order to verify the accuracy of the algorithm, the CAV-H is used as the reentry vehicle model to carry out simulations under seven different target states. Simulations are performed in seven different target states. Reentry initial state is h 0 = 60km, V 0 =7200m / s, λ 0 = 0°, θ 0 = 45°, γ 0 = 0°. ψ 0 Take the value according to the target direction. Ballistic damping control technology is used to suppress ballistic oscillation, where the ballistic damping feedback item coefficient K γ =5. terminal bound to E TAEM =-5.5×10 7 J / kg. Simulation results such as Figure 5-Figure 6 .
[0550] Table 1 Terminal state quantity
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[0554] Figure 5 In , the trajectory of the eastward flight is curved due to the influence of the Coriolis force. from Figure 5 and Image 6 It can be seen from the simulation results that the accuracy of the new analytical solution is also very high in the general case where the lift-to-drag ratio...
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