Trajectory analysis of a dual-spin-stabilized projectile with fixed-canards for the precision guidance kit

Author:

Shi Kai12ORCID,Liu Mabao12ORCID

Affiliation:

1. State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi’an Jiao Tong University, Xi’an, PR China

2. School of Aerospace, Xi’an Jiao Tong University, Xi’an, PR China

Abstract

The dual-spin-stabilized projectile’s mechanism of angular motion is analyzed, taking into account the two pairs of fixed-canards. Based on the non-homogeneous terms of the angle of attack (AOA) equation, the gyroscopic stability and precession feature of a double-spinning projectile are theoretically analyzed. The negative AOA is unraveled under the influence of two pairs of fixed-canards. Furthermore, the dual-spin-stabilized projectile’s angular movements, with the lift-canards fixed at different directions, are described; thus, the phenomenon is revealed whereby the deflection of the lift-canards is opposite to that of the projectile correction direction. Then, the Monte Carlo trajectory simulation is used to verify the angular motion law of a dual-spin-stabilized projectile with fixed-canards. The results of the analysis offer a meaningful strategy to control a class of dual-spin-stabilized projectiles that is not limited to the fixed-canard type.

Funder

Aeronautical Science Foundation of China

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

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