hello everybody:
me and my freind are designing an altitude control circuit using an MCU and a 40KHz ultrsound sensor, but we had a problem in analyising the transfer function of the airplane altittude system, where we found out that it's a multi input (thrust +elevator deflection angle) and multi output (velocity +altitude+pitch angle) system.
so if there's anyone who can help us with the TF, cause we treid to convert the inputs and outputs to mathematics but we didn't get anything useful.
so plz help us even by a simple and good advice.
me and my freind are designing an altitude control circuit using an MCU and a 40KHz ultrsound sensor, but we had a problem in analyising the transfer function of the airplane altittude system, where we found out that it's a multi input (thrust +elevator deflection angle) and multi output (velocity +altitude+pitch angle) system.
so if there's anyone who can help us with the TF, cause we treid to convert the inputs and outputs to mathematics but we didn't get anything useful.
so plz help us even by a simple and good advice.