International Journal of Aerospace Engineering / 2015 / Article / Tab 1

Research Article

Decentralized State Estimation Algorithm of Centralized Equivalent Precision for Formation Flying Spacecrafts Based on Junction Tree

Table 1

Keplerian orbital elements of a satellite formation.

Sat number (km) (°) (°) (°) (°)

18400.0000000.00500030.000000120.0000000.00000090.000000
28400.0000000.00474329.996649119.9881511.78313888.250782
38400.0000000.00474330.003353120.0118471.76261688.250782