Chinese Space Science and Technology
• • Previous Articles Next Articles
Wang Guangmin (Beijing Aerospace Automatic Control Institute)
Online:
Abstract: This paper presents a calculation method by utilizing telemetric integral data of accelerometer about some particular points (such as cutoff point, orbit injection point etc) of launch rocket to calculate trajectory parameters and orbital elements of such points.
Wang Guangmin (Beijing Aerospace Automatic Control Institute). USING INTEGRAL TELEMETRIC DATA OF ACCELEROMETER TO CALCULATE TRAJECTORY PARAMETERS AND ORBITAL ELEMENTS[J]. Chinese Space Science and Technology.
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: https://journal26.magtechjournal.com/kjkxjs/EN/
https://journal26.magtechjournal.com/kjkxjs/EN/Y1990/V10/I03/42
