Design and development of a spacecraft control algorithm

The problem of spacecraft control in flight along a given trajectory is investigated. Spacecraft dynamics is described by a non-stationary model, which parameters are not reliably known. Control algorithms are developed using linear stationary and non-stationary models. Method for generating the non...

Full description

Saved in:
Bibliographic Details
Main Authors: Afanasyev, V. N., Neusypin, K. A.
Format: Conference Proceeding
Language:English
Subjects:
Algorithms
Control theory
Mathematical models
Optimization
Parameters
Spacecraft
Spacecraft control
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:The problem of spacecraft control in flight along a given trajectory is investigated. Spacecraft dynamics is described by a non-stationary model, which parameters are not reliably known. Control algorithms are developed using linear stationary and non-stationary models. Method for generating the non-stationary control system optimization algorithms based on using the Hamilton – Jacobi equation and the Pontryagin minimum principle is considered. Control algorithm with non-stationary model optimization parameters is constructed.
ISSN:0094-243X
1551-7616
DOI:10.1063/5.0111112