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Hi, I had modelled an aeroelastic wing and obtained the state-space(A,B,C,D) of the linearised system. Is it possible in SHARPy where i can obtain the states value (\eta \zeta) can calculate the control surface deflection all within the DynamicCoupled Solvers? I am doing this for gust load alleviation purposes. Thank you! |
Replies: 2 comments 8 replies
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Hi, I'm not sure if I exactly follow what you are trying to achieve. I assume that by value of the states you refer to a time domain simulation, if so, I would recommend you simulate the linear time domain system externally to SHARPy (i.e. using Hope this helps |
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https://github.com/ImperialCollegeLondon/sharpy/tree/fix_udp_crv |
Hi,
I'm not sure if I exactly follow what you are trying to achieve. I assume that by value of the states you refer to a time domain simulation, if so, I would recommend you simulate the linear time domain system externally to SHARPy (i.e. using
scipy.signal.dlsim()or Matlab). The typical output of a linear time domain simulation from these functions is the outputyand also the statesxof the system. In SHARPy, theDynamicCoupledsolver is intended for nonlinear time-domain simulations.Hope this helps