BROWSE
Detail
Registered METHOD FOR FAST AND PRECISE ORBIT PROPOGATION INCLUDING MANEUVER
- Inventors
- Hwang Yoola, Lee Byoung-Sun, Lee Soo Jeon, Kim Jae Hoon
- Application No.
- 13334988 (2011.12.22)
- Publication No.
- 20120166084 (2012.06.28)
- Registration No.
- 8600676 (2013.12.03)
- Country
- UNITED STATES
- Project Code
- 10MR1700, Study on Space Qualification of Ka band Payload and Application Technology for COMS, Do-Seob Ahn
- Abstract
- A flight dynamics subsystem (FDS), a velocity increment calculation module, and operational methods of the same are provided. A used fuel quantity actually used in a satellite is calculated, and a velocity increment is calculated using the calculated fuel quantity. Therefore, an orbit of the satellite may be estimated more accurately.
- KSP Keywords
- Velocity increment, flight dynamics
- Family
| Status | Patent | Country | KIPRIS |
|---|---|---|---|
| Registered | 매뉴버를 포함하는 빠르고 정확한 궤도 전파 방법 | KOREA | KIPRIS |