Optimal Maneuver Trajectory for Hypersonic Missiles in Dive Phase Using Inverted Flight
To determine the optimal trajectory for the dive phase of a hypersonic missile, a maneuver strategy using inverted flight is presented. The combat scene that the hypersonic missile attacks the fixed target on the ground is considered in this paper. Particularly, a maneuvering form named inverted fli...
Main Authors: | Shili Tan, Humin Lei, Tao Liu |
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Format: | Article |
Language: | English |
Published: |
IEEE
2019-01-01
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Series: | IEEE Access |
Subjects: | |
Online Access: | https://ieeexplore.ieee.org/document/8713451/ |
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