GB/T 14410.1-1993
Replaced
GB/T 32300-2015
Active
National standards
GB/T 32300-2015 Best practices for orbit elements at payload-launch vehicle separation
GB/T 32300-2015 Best practices for orbit elements at payload-launch vehicle separation
Basic Information
Standard Code:
GB/T 32300-2015
Standard Type:
National standards
Standard Status:
Active
is_force_gb:
no
CCS Name:
\n Spacecraft control and guidance system
ICS Name:
Integrated aircraft and spacecraft
Publish Date:
2015-12-31
Implement Date:
2016-07-01
Pages:
14 pages
Scope
This standard specifies the calculation method for the orbital elements of the separation point of the launch vehicle and the payload, including the orbital elements and calculation conditions, the calculation method for the orbital elements, and the calculation method for the error of the orbital elements. This standard is applicable to the calculation method of the orbital elements of different payloads such as satellites, manned spacecraft, and space stations, and is applicable to different orbits such as low Earth orbit, sun-synchronous orbit, medium Earth orbit, geosynchronous transfer orbit, and geosynchronous orbit.
Development Information
Referenced Standards
ANSI/AIAA S-131-2010
CCSDS 500.0-G-3
Related Standards
GB/T 14410.2-1993
Replaced
GB/T 14410.2-1993 Flight mechanics—Concepts,quantities and symbols Forces, moments, their coefficients and derivatives
GB/T 14410.3-1993
Replaced
GB/T 14410.3-1993 Flight mechanics—Concepts,quantities and symbols—Stability and control of aircraft
GB/T 14410.4-1993
Replaced
GB/T 14410.4-1993 Flight mechanics—Concepts,quantities and symbols—Flight performance
GB/T 14410.5-1993
Replaced
GB/T 14410.5-1993 Flight mechanics—Concepts,quantities and symbols—Flight measurements
GB/T 14410.6-1993
Replaced