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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
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2014
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Article
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Tab 2
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Research Article
Active Disturbance Rejection Station-Keeping Control of Unstable Orbits around Collinear Libration Points
Table 2
Initial orbits parameters of Halo missions without injection errors.
Mission orbits
ISEE-3 (110,000 km)
0.988872932669558
0
0
0.008853797264729
0
Halo (800,000 km)
0.989390221855232
0
0.006248517078177
0
0.012547011257083
0