Determination of a pitch control program for a solid-propellant missile

This paper analyzes the trends in the improvement of the performance characteristics of guided missiles with solid-propellant sustainer engines and identifies the features and requirements for flight trajectories, design parameters, and control programs. Within the framework of the optimal control t...

Full description

Saved in:
Bibliographic Details
Published in:Technical mechanics Vol. 2023; no. 3; pp. 18 - 34
Main Author: Siutkina-Doronina, S.V.
Format: Journal Article
Language:English
Published: 19.10.2023
ISSN:1561-9184, 2616-6380
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Be the first to leave a comment!
You must be logged in first