QJ 1997A-2014
Simulation calculation for flying trajectory simulation of ballistic missile and launch vehicle (English Version)

Standard No.

QJ 1997A-2014

Language

Chinese, Available in English version

Release Date

2014

Published By

Professional Standard - Aerospace

Replace

QJ 1997-1990

Scope

This standard specifies the calculation method for mathematical simulation of ballis ic mis iles and launch vehicles in the launch point normal inertial coordinate system. This standard applies to ballis ic simulation calculations during the design process of ballis ic mis ile and launch vehicle guidance systems. Ballis ic simulation calculations of other systems can be used as a reference.

QJ 1997A-2014 Referenced Document

• GJB 3588 missile control system terminology
• GJB 365.1-1987 Northern Hemisphere standard atmosphere (-2~80 kilometers)
• GJB 6304-2008 China geodetic system 2000
• QJ 1028B-2008 Commonly used coordinate systems for aerospace products
• QJ 1215 missile general term

QJ 1997A-2014 history

• 1990 QJ 1997-1990 Simulation Calculation of Flight Trajectories of Ballistic Missiles and Launch Vehicles

QJ 1997A-2014 Simulation calculation for flying trajectory simulation of ballistic missile and launch vehicle has been changed from QJ 1997-1990 Simulation Calculation of Flight Trajectories of Ballistic Missiles and Launch Vehicles.