Longitudinal Control System Design Using Gradient Method for a Suborbital Launcher-Reference-Cited by-同舟云学术

Longitudinal Control System Design Using Gradient Method for a Suborbital Launcher

Published:2014-06 Issue: Volume:555 Page:113-120
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Chelaru Teodor Viorel¹,Pana Valentin¹,Chelaru Adrian²

Affiliation:

1. University POLITEHNICA of Bucharest

2. National Institute for Aerospace Research “elie Carafoli”

Abstract

The aim of this paper is to present a design method for the guidance navigation and control system (GNC) of a suborbital launcher. In order to achieve a symmetric evolution in the vertical plane we start with the decoupled form of the equation of motion. Afterwards these equations are linearized and the extended stability and command matrices are constructed by adding some auxiliary equations. The linear control law is obtained and the control matrix containing the unknown coefficients is presented. The design of the control system is based on a modified gradient method. To illustrate the proposed method the synthesis of the control system in the specific case of the SLT ("Suborbital Launcher for Testing - SLT" financed thru „Programme for Research-Development-Innovation on Space Technology and Advanced Research – STAR”) is presented.

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.555.113.pdf

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