Research Article

Hardware-in-the-Loop Simulation for Spacecraft Formation Flying

Figure 6

Simulation results using Fuzzy Logic control (control interval: 1000 seconds; maximum firing time: 2 seconds).
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(a) Three-dimensional relative trajectory
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(b) Position error in 𝑥 -axis
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(c) Position error in 𝑦 -axis
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(d) Position error in 𝑧 -axis
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(e) Control signal in 𝑥 -axis
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(f) Control signal in 𝑦 -axis
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(g) Control signal in 𝑧 -axis