Optimal Maneuver Trajectory for Hypersonic Missiles in Dive Phase Using Inverted Flight

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...

Full description

Bibliographic Details
Main Authors: Shili Tan, Humin Lei, Tao Liu
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Trajectory optimization
hypersonic missile
inverted flight
pseudospectral method
mesh refinement
Online Access:https://ieeexplore.ieee.org/document/8713451/

Internet

https://ieeexplore.ieee.org/document/8713451/

Similar Items