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en:sim_earth [2018/01/29 14:22] ashley |
en:sim_earth [2020/03/25 16:28] (current) |
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*control system for "ground" telemetry stations and a photodiode for detecting the light | *control system for "ground" telemetry stations and a photodiode for detecting the light | ||
- | All the geometric parameters of the globe, the kinematic parameters of its rotation, as well as [[pendant|satellite gimbal]], and the onboard payload capabilities (field of view, exposure time, light conditions, data transmission speed) used in the model for obtaining special information are coordinated with the dynamic on-board control system capabilities of the satellite model (speed, accuracy, number of degrees of freedom, time of continuous operation). | + | All the geometric parameters of the globe, the kinematic parameters of its rotation, the [[pendant|satellite gimbal]], and the onboard payload capabilities (field of view, exposure time, light conditions, data transmission speed) used in the model for obtaining special information are coordinated with the dynamic on-board control system capabilities of the satellite model (speed, accuracy, number of degrees of freedom, time of continuous operation). |
- | Task list formulated for working groups to solve using the stand should also be coordinated with the possibilities and limitations of the "stand + model" system and take into account possible known, well-defined, clearly stated restrictions. These restrictions, however, should not influence the "physicality" of the phenomena and principles underlying the theory and practice of controlling a real satellite in a near-earth orbit. | + | The task list formulated for working groups to solve using the stand should be created keeping the possibilities and limitations of the "stand + model" system in mind. The list should take into account known, well-defined, clearly-stated restrictions. These restrictions, however, should not influence the "physicality" of the phenomena and principles underlying the theory and practice of controlling a real satellite in a near-earth orbit. |
- | The "stand + model" system should also allow the variation of the initial conditions during the experiment, thereby providing users with different versions of tasks of the same complexity and the choice of several alternative ways to solve the task. | + | The "stand + model" system should also allow for the variation of initial conditions during the experiment, thereby providing users with different versions of tasks of the same complexity and the choice of several alternative ways to solve the said task. |