Research Article

Autonomous Orbit Determination for Lagrangian Navigation Satellite Based on Neural Network Based State Observer

Table 1

Initial state of the Lagrangian satellites.

SatellitesS1S2S3S4

0.0571173803026270.0631165787484190.018916778218648
0.000050795432543
0.0712425409157780.0777240379101680.0433772722156990.030872891241568
0.0252372534222370.0444327039774820.002938265403217
0.0247681429666890.0921258807184520.011290787920073