CSMP III Program for Autopilot Aircraft System

TITLE AIRCRAFT WITH RATE CONTROL
*
PARAM D = (5.656, 16.968, 39.592, 56.56, 113.12)
INPUT = ATIME ERROR = INPUT – HEAD TORQUE = KERROR – D*ANGVEL
ANGACC = TORQUE/I
HEAD = INTGRL (0.0, ANGVEL)
ANGVEL= INTGRL (0.0, ANGACC)
*
CONST I = 2.0, K = 400.0, A = 0.0175
TIMER DELT = 0.005, FINTIM = 1.5, PRDEL = 0.05
PRINT HEAD
LABEL HEADING VERSUS TIME
END

Note: 𝜽𝟎, 𝜽𝟎 𝒂𝒏𝒅 𝜽𝟎 are HEAD, angular velocity (ANGVEL) and angular
acceleration (ANGACC respectively). A is constant. D takes different values on
five separate runs

 

Ashok Nath

Ashok Nath is a content creator in easytipstutorial.com and he is pursuing Bachelor's Degree In Computer Engineering From Nepal College Of Information Technology (NCIT) Pokhara University Nepal. He like to write tips and tutorials on different kinds of difficulties that people would face on thier way to success.

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