Comparative Analysis between Two Trajectory Models of Sinusoidal Maneuvering Missiles

Abstract:

For the sinusoidal maneuvering missile, its important but difficulty to distinguish the Base Course with Constant Velocity Model and the Tangential Arcs Model as the trajectory model. Their similarities and differences are studied to find out the selection method firstly, and their mathematical models are set up in the base-course coordinate system based on the existing references. Using the kinematical equations, the control complexities are derived. Then with the premise of same amplify, same max tangential velocity, same base-course pitch, their overloads and plane trajectories are compared, and drawn out some useful conclusions, such as TA model should be the prior selection for route planning, while BCCV model could be its approximate solution under certain conditions.

• Periodical: Applied Mechanics and Materials (Volumes 475-476)
• Pages: 616-620
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.475-476.616
• Online since: December 2013
• Authors: Qiang Fu, Chun Ping Wang
• Keywords: Base Course, Mathematical Models, Overload, Sinusoidal Maneuver

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