Recommended Practice AIAA/ANSI R-004-1992 Recommended Practice for Atmospheric and Space Flight Vehicle Coordinate Systems AIAA standards are copyrighted by the American Institute of Aeronautics and Astronautics (AIAA), 1801 Alexander Bell Drive, Reston, VA 20191-4344 USA. All rights reserved. AIAA grants you a license as follows: The right to download an electronic file of this AIAA standard for temporary storage on one computer for purposes of viewing, and/or printing one copy of the AIAA standard for individual use. Neither the electronic file nor the hard copy print may be reproduced in any way. In addition, the electronic file may not be distributed elsewhere over computer networks or otherwise. The hard copy print may only be distributed to other employees for their internal use within your organization.
Recommended Practice forAtmospheric and Space Flight Vehicle
Coordinate Systems
AIAA standards are copyrighted by the American Institute of
Aeronautics andAstronautics (AIAA), 1801 Alexander Bell Drive,
Reston, VA 20191-4344 USA. All rightsreserved.
AIAA grants you a license as follows: The right to download an
electronic file of this AIAAstandard for temporary storage on one
computer for purposes of viewing, and/or printingone copy of the
AIAA standard for individual use. Neither the electronic file nor
the hardcopy print may be reproduced in any way. In addition, the
electronic file may not bedistributed elsewhere over computer
networks or otherwise. The hard copy print may onlybe distributed
to other employees for their internal use within your
organization.
American Institute ofAeronautics and Astronautics
1801 Alexander Bell Drive, Suite 500Reston, VA 20191-4344
ISBN 1-56347-285-6ISBN 1-56347-416-6
AbstractTable of ContentsForeword1.0 Introduction1.1 Axis
systems1.2 Positions1.3 Angles1.4 Velocities and angular
velocities1.5 Flight vehicle inertia, reference quantities, and
reduced parameters1.6 Forces, moments, coefficients, and load
factors1.7 Thrust, resultant moment of propulsive forces, airframe
aerodynamic force, airframe aerodynamic moment, and their
component1.8 Coefficients for the components of the thrust1.9
Forces and moments involved in the control of the flight
vehicle1.10 Forces and moments acting on the motivators1.11
Quantities related to energyAppendix AAppendix BAppendix CAppendix
DAppendix E
