Research Article
A Rapid Target Searching Scheme for a Small Satellite with Device Limits
Table 1
Total mission time of both initial attitude estimation mode and target searching mode in different initial condition settings.
| Initial disturbance angles | NAM | 2°/s | 5°/s | 10°/s |
| 2°, [0 0 -1] | 0 | 24.3 s | 23.7 s | 23.4 s | 5°, [0 0 -1] | 1 | 26.4 s | 26.0 s | 25.6 s | 5°, [0 -0.78 -0.62] | 2 | 28.8 s | 28.5 s | 28 s | 5°, [0 -0.97 0.22] | 3 | 31.9 s | 31.3 s | 31.3 s | 5°, [0 -0.43 0.90] | 4 | 34.0 s | 33.7 s | 33.5 s | 5°, [0 0.43 0.90] | 5 | 36.5 s | 36.6 s | 36.2 s | 5°, [0 0.97 0.22] | 6 | 39.3 s | 38.4 s | 38.8 s | 5°, [0 0.78 -0.62] | 7 | 41.9 s | 41.3 s | 41.4 s |
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