Research Article
Guidance Navigation and Control for Autonomous Multiple Spacecraft Assembly: Analysis and Experimentation
Table 2
Main simulation parameters.
| Mass of each simulator | 10,5 | kg |
| Inertia of simulator | 0.063 | kg m2 | Inertia of the two simulators assembled | 0.18 | kg m2 | Single thruster estimated force [36] | 0.16 | | Docking cone semiaperture | 0.75 | degrees | Force arms (for torque generation) | 5, 10, 21 | cm | Limit distance for switching off the thrusters | 0.7 | m | iGPS accuracy | 1 | mm | Gyroscope accuracy | 0.003 | deg/sec | Thrusters minimum actuation time | | sec |
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