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📄 gravity.htm

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    <title>
      FDC help: Gravity
    </title>
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  <body bgcolor="#DDDDDD"><div>
    <h2>
      Subsystem <i>Gravity</i>
    </h2>
    <p><i>Gravity</i> computes the gravitational force components
    along the aircraft&#39;s body axes. The
    acceleration of gravity, <i>g</i>, is extracted from the outputvector of <i><a href="atmosph.htm">Atmosph</a></i>. The outputs from
    <i>Gravity</i> are sent to the block <i><a href=
    "fmsort.htm">FMsort</a></i>. </p>
    <h3>
      Inputvectors: <i>x</i> and <i>yatm</i>
    </h3>
<pre>
  x    = [V alpha beta p q r psi theta phi xe ye H]&#39;     (states)
  yatm = [rho ps T mu g]&#39;   (atmospheric properties, computed in
                                               the block <a href=
"atmosph.htm">Atmosph</a>)

 {V    : airspeed [m/s]                                         }
 {alpha: angle of attack [rad]                                  }
 {beta : sideslip angle [rad]                                   }
 {p    : roll rate [rad/s]                                      }
 {q    : pitch rate [rad/s]                                     }
 {r    : yaw rate [rad/s]                                       }
 {psi  : yaw angle [rad]                                        }
  theta: pitch angle [rad]
  phi  : roll angle [rad]
 {xe   : x-coordinate in Earth-fixed reference frame [m]        }
 {ye   : y-coordinate &#39;&#39;     &#39;&#39;          &#39;&#39;      &#39;&#39;  [m]        }
 {H    : altitude above sea-level [m]                           }

 {rho  : airdensity [kg/m^3]                                    }
 {ps   : static pressure [N/m^2]                                }
 {T    : temperature [K]                                        }
 {mu   : dynamic viscosity [kg/(m*s)]                           }
  g    : acceleration of gravity [m/s^2]
</pre>
    The inputsignals which are not actually used by <i>Gravity</i> have been
    put between curly braces. 
    <h3>
      Outputvector: <i>Fgrav</i>
    </h3>
<pre>
  Fgrav = [Xgr Ygr Zgr]&#39;.

  Xgr, Ygr, Zgr: gravity force components along the aircraft&#39;s
                 body-axes [N].
</pre>
    <h3>
      Parameters to be defined in the Matlab Workspace.
    </h3>
    <p><i>GM1</i>: vector with some important geometrical properties of the
    &#39;Beaver&#39; aircraft, and its mass (which is assumed to be constant
    during the motions of interest). Here, the mass <i>m</i> is extracted from
    <i>GM1</i>. The vector <i>GM1</i> can be loaded into the workspace from
    file by running the utility <i><a href="datload.htm">DATLOAD</a></i>. Run
    <i><a href="modbuild.htm">MODBUILD</a></i> first if the datafile does not
    yet exist.</p>
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