NASA-LLIS-0692

Lessons Learned – Coordinate Systems for Attitude Determination and Control

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:30:57Z
date available	2017-09-04T17:30:57Z
date copyright	03/13/2000
date issued	2000
identifier other	CWCEQCAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/153877
description abstract	Practice: This guideline provides a procedure which specifies and documents consistent, useful, and welldefined coordinate system (or frame) definitions for spacecraft attitude control design and analysis. Several example coordinate frames and transformations are presented to show how these definitions are used to address various Attitude Control System (ACS) design issues. Past experience has shown the most efficient convention varies from project to project as a function of mission type, constraints, and performance requirements. This procedure addresses the process and documentation to reliably define the most efficient reference frame convention for a given mission or spacecraft.
language	English
title	NASA-LLIS-0692	num
title	Lessons Learned – Coordinate Systems for Attitude Determination and Control	en
type	standard
page	9
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2000
contenttype	fulltext