Main Catalog Aviation and Rocket-Space Engineering Aircraft Dynamics, Ballistics, Motion Control

Analytic investigation of the approaches to increasing the navigational accuracy of the pulse-corrected aircraft

Authors: Vedenichev I.V.
Published in issue: #7(24)/2018
DOI: 10.18698/2541-8009-2018-7-341
Category: Aviation and Rocket-Space Engineering \| Chapter: Aircraft Dynamics, Ballistics, Motion Control
Keywords: ballistic analysis, pulse correction, accuracy increase, corrected missile, low trajectory, high trajectory, MATLAB, Simulink, flight simulation
Published: 24.07.2018

The article provides the results of computational investigations devoted to the research of the on-board coordinator’s minimum viewing angle and the vernier engine thrust impact on the navigational accuracy of the corrected aircraft. We compare the aircraft correction accuracy when moving along the low and high trajectories and give a qualitative estimate of the results obtained. The work presents the analysis of using two different algorithms for determining the corrected flight starting point.

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