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Georgia Institute Of TechnologyCS 6440RocketPIDStudent.py
- Summary • 3 pages • 2021
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# Optimize your PID parameters here: pressure_tau_p = 0.1 pressure_tau_d = 1.0 rocket_tau_p = 2.0 rocket_tau_i = 12 rocket_tau_d = 0.005 def pressure_pd_solution(delta_t, current_pressure, data) : """Student solution to maintain LOX pressure to the turbopump at a level of 100. Args: delta_t (float): Time step length. current_pressure (float): Current pressure level of the turbopump. data (dict): Data passed through out run. Additional data can be added and existing values modified. 'ErrorP'...
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