**Standard Simulation Variable Names**

Modeling and Simulation Technical Committee

August 2006

This table is meant to contain simulation variables that are independent
of the particular vehicle type being simulated. These variables are
tailored towards aircraft simulation.

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<col style="width: 8%" />
<col style="width: 21%" />
<col style="width: 23%" />
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</colgroup>
<thead>
<tr class="header">
<th></th>
<th><strong>Symbol</strong></th>
<th><strong>Short Name</strong></th>
<th><strong>Full Variable Name</strong></th>
<th><strong>Description</strong></th>
<th><strong>Sign Convention</strong></th>
<th><strong>Intial Value</strong></th>
<th><strong>Min Value</strong></th>
<th><strong>Max Value</strong></th>
<th></th>
<th><strong>Note</strong></th>
<th><strong>Date Changed</strong></th>
</tr>
</thead>
<tbody>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td><p><mark>eulerAngle_d(3)</mark></p>
<p><mark>eulerAngle_r(3)</mark></p>
<p><mark>(euler_angle_d(3))</mark></p></td>
<td><mark>Vector of the roll, pitch, and yaw Euler angles defined
below</mark></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>1</td>
<td>Φ</td>
<td>PHI</td>
<td><p>rollEulerAngle_d</p>
<p>rollEulerAngle_r</p>
<p>(roll_euler_angle_d)</p></td>
<td>Roll Euler Angle, FE (flat earth or local) Frame</td>
<td>RWD</td>
<td></td>
<td>-180</td>
<td>180</td>
<td></td>
<td>2</td>
<td></td>
</tr>
<tr class="odd">
<td>2</td>
<td>θ</td>
<td>THET</td>
<td><p>pitchEulerAngle_d</p>
<p>pitchEulerAngle_r</p></td>
<td>Pitch Euler Angle, FE (flat earth or local) Frame</td>
<td>ANU</td>
<td></td>
<td>-90</td>
<td>90</td>
<td></td>
<td>2</td>
<td></td>
</tr>
<tr class="even">
<td>3</td>
<td>ς</td>
<td>PSI</td>
<td><p>yawEulerAngle_d</p>
<p>yawEulerAngle_r</p></td>
<td>Yaw Euler Angle, FE (flat earth or local) Frame</td>
<td>ANR</td>
<td></td>
<td>-180</td>
<td>180</td>
<td></td>
<td>2</td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td><p><mark>eulerAngleRate_d(3)</mark></p>
<p><mark>eulerAngleRate_r(3)</mark></p>
<p><mark>(euler_angle_rate_d(3))</mark></p></td>
<td><mark>Vector of the roll, pitch, and yaw Euler angle rates defined
below</mark></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>7</td>
<td>p</td>
<td>PHID</td>
<td>rollEulerAngleRate_rs-1</td>
<td>Euler roll rate, FE (flat earth or local) frame</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>8</td>
<td>q</td>
<td>THED</td>
<td>pitchEulerAngleRate_rs-1</td>
<td>Euler pitch rate, FE (flat earth or local) frame</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>9</td>
<td>r</td>
<td>PSID</td>
<td>yawEulerAngleRate_rs-1</td>
<td>Euler yaw rate, FE (flat earth or local) frame</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>10</td>
<td></td>
<td>SPHI</td>
<td>rollEulerAngleSine</td>
<td>Sine Of Euler Roll Angle</td>
<td>RWD</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>11</td>
<td></td>
<td>CPHI</td>
<td>rollEulerAngleCosine</td>
<td>Cosine Of Euler Roll Angle</td>
<td>RWD</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>12</td>
<td></td>
<td>STHT</td>
<td>pitchEulerAngleSine</td>
<td>Sine Of Euler Pitch Angle</td>
<td>ANU</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>13</td>
<td></td>
<td>CTHT</td>
<td>pitchEulerAngleCosine</td>
<td>Cosine Of Euler Pitch Angle</td>
<td>ANU</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>14</td>
<td></td>
<td>SPSI</td>
<td>yawEulerAngleSine</td>
<td>Sine Of Euler Yaw Angle</td>
<td>ANR</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>15</td>
<td></td>
<td>CPSI</td>
<td>yawEulerAngleCosine</td>
<td>Cosine Of Euler Yaw Angle</td>
<td>ANR</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>TEToB(3,3)</td>
<td>The FE to Body transformation matrix composed of the elements
defined below</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>16</td>
<td></td>
<td>T11</td>
<td>FEToBT11</td>
<td>CTHT*CPSI (FE To B) axis transformation element</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>17</td>
<td></td>
<td>T21</td>
<td>FEToBT21</td>
<td>SPHI*STHT*CPSI - CPHI*SPSI (FE To B) axis transformation
element</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>18</td>
<td></td>
<td>T31</td>
<td>FEToBT31</td>
<td>CPHI*STHT*CPSI + SPHI*SPSI (FE to B) axis transformation
element</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>19</td>
<td></td>
<td>T12</td>
<td>FEToBT12</td>
<td>CTHT*SPSI (FE to B) axis transformation element</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>20</td>
<td></td>
<td>T22</td>
<td>FEToBT22</td>
<td>SPHI*STHT*SPSI + CPHI*CPSI (FE to B) axis transformation
element</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>21</td>
<td></td>
<td>T32</td>
<td>FEToBT32</td>
<td>CPHI*STHT*SPSI - SPHI*CPSI (FE to B) axis transformation
element</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>22</td>
<td></td>
<td>T13</td>
<td>FEToBT13</td>
<td>-STHT (FE to B) axis transformation element</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>23</td>
<td></td>
<td>T23</td>
<td>FEToBT23</td>
<td>SPHI*CTHT (FE to B) axis transformation element</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>24</td>
<td></td>
<td>T33</td>
<td>FEToBT33</td>
<td>CPHI*CTHT (FE to B) axis transformation element</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>25</td>
<td></td>
<td>ALFA</td>
<td><p>angleOfAttack_d</p>
<p>angleOfAttack_r</p></td>
<td>Angle Of Attack, Body axis</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>26</td>
<td></td>
<td>BETA</td>
<td><p>angleOfSideslip_d</p>
<p>angleOfSildesip_r</p></td>
<td>Sideslip Angle, Body axis</td>
<td>ANL</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>29</td>
<td></td>
<td>ALFD</td>
<td>angleOfAttackRate_rs-1</td>
<td>Angle Of Attack Rate, Body axis</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>30</td>
<td></td>
<td>BETD</td>
<td>angleOfSideslipRate_rs-1</td>
<td>Sideslip Angle Rate</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>31</td>
<td></td>
<td>SALPH</td>
<td>sineAngleOfAttack</td>
<td>Sine Of Angle Of Attack</td>
<td>ANU</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>32</td>
<td></td>
<td>CALPH</td>
<td><p>cosineAngleOfAttack</p>
<p>(cosine_angle_of_attack)</p></td>
<td>Cosine Of Angle Of Attack</td>
<td>ANU</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>33</td>
<td></td>
<td>SBETA</td>
<td><p>sineAngleOfSideslip</p>
<p>(sine_angle_of_attack)</p></td>
<td>Sine Of Sideslip Angle</td>
<td>ANL</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>34</td>
<td></td>
<td>CBETA</td>
<td><p>cosineAngleOfSideslip</p>
<p>(cosine_angle_of_sideslip)</p></td>
<td>Cosine Of Sideslip Angle</td>
<td>ANL</td>
<td></td>
<td>-1.0</td>
<td>1.0</td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>35</td>
<td>γ<sub>V</sub></td>
<td>GAMV</td>
<td><p>flightPathAngle_r</p>
<p>flightPathAngle_d</p>
<p>(flight_path_angle_r)</p></td>
<td>Flight Path Angle Above Horizon</td>
<td>ANU</td>
<td></td>
<td>-p/2</td>
<td>p/2</td>
<td>10) 1.3.5.2</td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td>36</td>
<td>γ<sub>H</sub></td>
<td>GAMH</td>
<td><p>flightPathAzimuth_r</p>
<p>flightPathAzimuth_d</p>
<p>(flight_path_azimuth_r)</p>
<p><mark>(Ground_Track_Velocity_Angle)</mark></p></td>
<td>Flight Path Angle In Horizon Plane</td>
<td>CWFN</td>
<td></td>
<td>-p</td>
<td>p</td>
<td>10) 1.3.5.1</td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td><p>s_bodyAngularRate_rs-1(3)</p>
<p>s_bodyAngularRate_ds-1(3)</p>
<p>(s_body_angular_rate_rs-1(3))</p></td>
<td>Vector of body axis angular rates comprised of the three components
as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>37</td>
<td>p</td>
<td>s_PB</td>
<td><p>s_bodyRollRate_rs-1</p>
<p>s_bodyRollRate_ds-1</p>
<p>(s_body_roll_rate_rs-1)</p></td>
<td>State, Aircraft Roll Velocity, Body Frame</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.4.6</td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td>38</td>
<td>q</td>
<td>s_QB</td>
<td>s_bodyPitchRate_rs-1 s_bodyPitchRate_ds-1
(s_body_pitch_rate_rs-1)</td>
<td>State, Aircraft Pitch Velocity, B-frame</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.4.6</td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td>39</td>
<td>r</td>
<td>s_RB</td>
<td>s_bodyYawRate_rs-1 s_bodyYawRate_ds-1 (s_body_yaw_rate_rs-1)</td>
<td>State, Aircraft Yaw Velocity, B-frame</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.4.6</td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td><p>sd_bodyAngularAcceleration_rs-2(3)</p>
<p>sd_bodyAngularAcceleration_ds-2(3)</p>
<p>(sd_body_angular_acceleration_rs-2(3))</p></td>
<td>Vector of body axis angular accelerations comprised of the three
components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>40</td>
<td>p</td>
<td>sd_PBD</td>
<td><p>sd_bodyRollAcceleration_rs-2</p>
<p>sd_bodyRollAcceleration_ds-2</p>
<p>(sd_body_roll_acceleration_rs-2)</p></td>
<td>State derivative, Aircraft Roll Acceleration, B-frame</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>41</td>
<td>q</td>
<td>sd_QBD</td>
<td><p>sd_bodyPitchAcceleration_rs-2</p>
<p>sd_bodyPitchAcceleration_ds-2</p>
<p>(sd_body_pitch_acceleration_rs-2)</p></td>
<td>State derivative, Aircraft Pitch Accel, B-frame</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>42</td>
<td>r</td>
<td>sd_RBD</td>
<td><p>sd_bodyYawAcceleration_rs-2</p>
<p>sd_bodyYawAcceleration_ds-2</p>
<p>(sd_body_yaw_acceleration_rs-2)</p></td>
<td>State derivative, Aircraft Yaw Acceleration, B-frame</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td><p>s_bodyVelocity_fs-1(3)</p>
<p>s_bodyVelocity_ms-1(3)</p>
<p>(s_body_velocity_fs-1(3))</p></td>
<td>Vector of body axis translational velocities comprised of the three
components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>43</td>
<td>U<sub>B</sub></td>
<td>s_UB</td>
<td><p>s_bodyXVelocity_fs-1</p>
<p>s_bodyXVelocity_ms-1</p>
<p>(s_body_x_velocity_fs-1)</p></td>
<td>State, X-velocity B-frame.</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.4.4</td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td>44</td>
<td>V<sub>B</sub></td>
<td>s_VB</td>
<td><p>s_bodyYVelocity_fs-1</p>
<p>s_bodyYVelocity_ms-1</p>
<p>(s_body_y_velocity_fs-1)</p></td>
<td>State, Y-velocity B-frame</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.4.4</td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td>45</td>
<td>W<sub>B</sub></td>
<td>s_WB</td>
<td><p>s_bodyZVelocity_fs-1</p>
<p>s_bodyZVelocity_ms-1</p>
<p>(s_body_z_velocity_fs-1)</p></td>
<td>State, Z-velocity B-frame</td>
<td>DWN</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.4.4</td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>bodyTurbulenceVelocity_fs-1(3) bodyTurbulenceVelocity_ms-1(3)
(body_turbulence_velocity_fs-1(3))</td>
<td>Vector of body axis translational turbulence velocities comprised of
the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>46</td>
<td>U<sub>TURB</sub></td>
<td>UTURB</td>
<td>bodyXTurbulenceVelocity_fs-1 bodyXTurbulenceVelocity_ms-1
(body_x_turbulence_velocity_fs-1)</td>
<td>X-velocity Turb. Component, B-frame</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>47</td>
<td>V<sub>TURB</sub></td>
<td>VTURB</td>
<td>bodyYTurbulenceVelocity_fs-1 bodyYTurbulenceVelocity_ms-1
(body_y_turbulence_velocity_fs-1)</td>
<td>Y-velocity Turb. Component, B-frame</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>48</td>
<td>W<sub>TURB</sub></td>
<td>WTURB</td>
<td>bodyZTurbulenceVelocity_fs-1 bodyZTurbulenceVelocity_ms-1
(body_z_turbulence_velocity_fs-1)</td>
<td>Z-velocity Turb. Component, B-frame</td>
<td>DWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td><p>FEVelocity_fs-1(3)</p>
<p>FEVelocity_ms-1(3)</p>
<p>(FE_velocity_fs-1(3))</p></td>
<td>Vector of Fixed Earth (FE) axis translational velocities comprised
of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>49</td>
<td>V<sub>N</sub></td>
<td>VN</td>
<td><p>FEXVelocity_fs-1</p>
<p>FEXVelocity_ms-1</p>
<p>(FE_x_velocity_fs-1)</p></td>
<td>Northward Velocity Over Fixed Earth (FE) axis system [flat,
non-rotating earth]</td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>50</td>
<td>v<sub>E</sub></td>
<td>VE</td>
<td><p>FEYVelocity_fs-1</p>
<p>FEYVelocity_ms-1</p>
<p>(FE_y_velocity_fs-1)</p></td>
<td>Eastward Velocity Over Fixed Earth (FE) axis system [flat,
non-rotating earth]</td>
<td>EAST</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>51</td>
<td>V<sub>D</sub></td>
<td>VD</td>
<td><p>FEZVelocity_fs-1</p>
<p>FEZVelocity_ms-1</p>
<p>(FE_z_velocity_fs-1)</p></td>
<td>Downward Velocity Toward Earth Ctr,.(FE) axis system [flat,
non-rotating earth]</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td><p>GEVelocity_fs-1(3)</p>
<p>GEVelocity_ms-1(3)</p>
<p>(GE_velocity_fs-1(3))</p></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>49</td>
<td>V<sub>N</sub></td>
<td>VNGE</td>
<td><p>GEXVelocity_fs-1</p>
<p>GEXVelocity_ms-1</p>
<p>(GE_x_velocity_fs-1)</p></td>
<td>Northward Velocity Over Geocentric Earth Fixed Axis System (GE)
[oblate spheroid rotating earth]</td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>50</td>
<td>v<sub>E</sub></td>
<td>VEGE</td>
<td><p>GEYVelocity_fs-1</p>
<p>GEYVelocity_ms-1</p>
<p>(GE_y_velocity_fs-1)</p></td>
<td>Eastward Velocity Over Geocentric Earth Fixed Axis System (GE)
[oblate spheroid rotating earth]</td>
<td>EAST</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>51</td>
<td>V<sub>D</sub></td>
<td>VDGE</td>
<td><p>GEZVelocity_fs-1</p>
<p>GEZVelocity_ms-1</p>
<p>(GE_z_velocity_fs-1)</p></td>
<td>Downward Velocity Toward Earth Center,Geocentric Earth Fixed Axis
System (GE) [oblate spheroid rotating earth]</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>52</td>
<td>V<sub>T</sub></td>
<td>VDOT</td>
<td>totalInertialAccel_fs-2 totalInertialAccel_ms-2
(total_inertial_accel_fs-2)</td>
<td>Rate of change of inertial velocity, FE (flat earth or local) frame
or GE frame, whichever applies</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>53</td>
<td>V<sub>T</sub></td>
<td>VT</td>
<td><p>totalInertialVelocity_fs-1 totalInertialVelocity_fs-1</p>
<p>(total_inertial_velocity_fs-1)</p></td>
<td>Total Velocity, FE (flat earth or local) frame or GE frame,
whichever applies</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>54</td>
<td>V<sub>RG</sub></td>
<td>VG</td>
<td><p>groundSpeed_fs-1</p>
<p>groundSpeed_ms-1</p>
<p>(ground_speed_fs-1)</p></td>
<td>Vehicle velocity relative to the ground, Ground Speed, FE (flat
earth or local) frame or GE frame, whichever applies. For GE frame,
groundspeed is relative to the gound location directly under the
aircraft.</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>55</td>
<td>V<sub>rw</sub></td>
<td>VRW</td>
<td><p>trueAirspeed_fs-1</p>
<p>trueAirspeed_ms-1</p>
<p>(true_airspeed_fs-1)</p></td>
<td>Vehicle Velocity relative to the wind (true airspeed)</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>56</td>
<td>M<sub>N</sub></td>
<td>XMACH</td>
<td><p>mach</p>
<p>(mach)</p></td>
<td>Mach Number of the aircraft</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>57</td>
<td>V<sub>NRW</sub></td>
<td>VNRW</td>
<td><p>velocityXRelativeToWind_fs-1</p>
<p>velocityXRelativeToWind_ms-1</p>
<p>(velocity_x_Relative_To_Wind_fs-1)</p></td>
<td><p>North Relative Velocity Vn-vnw</p>
<p>FE (flat earth or local) frame or GE frame, whichever applies. For GE
frame, groundspeed is relative to the gound location directly under the
aircraft.</p></td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>58</td>
<td>V<sub>ERW</sub></td>
<td>VERW</td>
<td><p>velocityYRelativeToWind_fs-1</p>
<p>velocityYRelativeToWind_ms-1</p>
<p>(velocity_y_Relative_To_Wind_fs-1)</p></td>
<td><p>East Relative Velocity Ve-vew</p>
<p>FE (flat earth or local) frame or GE frame, whichever applies. For GE
frame, groundspeed is relative to the gound location directly under the
aircraft.</p></td>
<td>EAST</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>59</td>
<td>V<sub>DRW</sub></td>
<td>VDRW</td>
<td><p>velocityZRelativeToWind_fs-1</p>
<p>velocityZRelativeToWind_ms-1</p>
<p>(velocity_z_Relative_To_Wind_fs-1)</p></td>
<td><p>Down Relative Velocity Vd-vdw</p>
<p>FE (flat earth or local) frame or GE frame, whichever applies. For GE
frame, groundspeed is relative to the gound location directly under the
aircraft.</p></td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>60</td>
<td>V<sub>EQ</sub></td>
<td>VEQ</td>
<td>equivalentAirspeed_nmih-1 (equivalent_airspeed_nmih-1</td>
<td>Equivalent Airspeed, nautical miles per hour</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) or Flat Earth (FE) translational
velocities comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>61</td>
<td>W<sub>N</sub></td>
<td>VNW</td>
<td><p>windXVelocity_fs-1</p>
<p>windXVelocity_ms-1</p>
<p>(wind_x_velocity_fs-1)</p></td>
<td><p>North component of wind velocity</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>TO</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>62</td>
<td>W<sub>E</sub></td>
<td>VEW</td>
<td><p>windYVelocity_fs-1</p>
<p>windYVelocity_ms-1</p>
<p>(wind_y_velocity_fs-1)</p></td>
<td><p>East component Of Wind Velocity</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>TO</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td><mark>63</mark></td>
<td><mark>W<sub>D</sub></mark></td>
<td><mark>VDW</mark></td>
<td><p><mark>WindZVelocity_fs-1</mark></p>
<p><mark>WindZVelocity_ms-1</mark></p>
<p><mark>(wind_z_velocity_fs-1)</mark></p>
<p><mark></mark></p></td>
<td><p><mark>Down Component Of Wind Velocity</mark></p>
<p><mark>FE (flat earth or local) frame or GE frame, whichever
applies.</mark></p></td>
<td><mark>TO</mark></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>64</td>
<td>W<sub>T</sub></td>
<td>VTW</td>
<td><p>windVelocity_fs-1</p>
<p>windVelocity_fs-1</p>
<p>(wind_velocity_fs-1)</p></td>
<td><p>Total Wind Velocity,</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>65</td>
<td>h</td>
<td>ALTD</td>
<td><p>altitudeRate_fs-1</p>
<p>altitudeRate_ms-1</p>
<p>(altitude_rate_fs-1)</p></td>
<td><p>Altitude Rate Of Change</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>66</td>
<td></td>
<td>XLOND</td>
<td><p>longitudeRate_rs-1</p>
<p>longitudeRate_ds-1</p>
<p>(longitude_rate_rs-1)</p></td>
<td><p>Longitude Rate Of Change</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>WEST</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>67</td>
<td></td>
<td>XLATD</td>
<td><p>latitudeRate_rs-1</p>
<p>latitudeRate_ds-1</p>
<p>(latitude_rate_rs-1)</p></td>
<td><p>Latitude Rate Of Change</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>68</td>
<td>h</td>
<td>ALT</td>
<td><p>altitudeMSL_f</p>
<p>altitudeMSL_m</p>
<p>(altitude_MSL_f)</p></td>
<td><p>Altitude Of Aircraft Above Sea Lvl</p>
<p>FE (flat earth or local) frame</p></td>
<td>UP</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>69</td>
<td></td>
<td>XLON</td>
<td><p><mark>GELongitude_r</mark></p>
<p><mark>GELongitude_d</mark></p>
<p><mark>FELongitude_r</mark></p>
<p><mark>FELongitude_d</mark></p>
<p><mark>(ge_longitude_r)</mark></p></td>
<td><p>Longitude Of Aircraft</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>WEST</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>70</td>
<td></td>
<td>XLAT</td>
<td><p>GELatitude_r</p>
<p>GELatitude_d</p>
<p>FELatitude_r</p>
<p>FELatitude_d</p>
<p>(ge_latitude_r)</p></td>
<td><p>Latitude Of Aircraft</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>71</td>
<td></td>
<td>SLAT</td>
<td><p>sineLatitude</p>
<p>(sine_latitude)</p></td>
<td><p>Sine Of Aircraft Latitude</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>72</td>
<td></td>
<td>CLAT</td>
<td><p>CosineLatitude</p>
<p>(Cosine_Latitude)</p></td>
<td><p>Cosine Of Aircraft Latitude</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) or Flat Earth (FE) translational
acclerations comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>73</td>
<td>V<sub>N</sub></td>
<td>VND</td>
<td><p>FEaxisXAccel_fs-2</p>
<p>FEaxisXAccel_ms-2 (FEaxis_x_accel_fs-2)</p>
<p>or</p>
<p>GEaxisXAccel_fs-2</p>
<p>GEaxisXAccel_ms-2 (GEaxis_x_accel_fs-2)</p></td>
<td><p>North Acceleration Over Earth</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>74</td>
<td>V<sub>E</sub></td>
<td>VED</td>
<td><p>FEaxisYAccel_fs-2</p>
<p>FEaxisYAccel_ms-2 (FEaxis_y_accel_fs-2)</p>
<p>or</p>
<p>GEaxisYAccel_fs-2</p>
<p>GEaxisYAccel_ms-2 (GEaxis_y_accel_fs-2)</p></td>
<td><p>East Acceleration Over Earth</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>EAST</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>75</td>
<td>V<sub>D</sub></td>
<td>VDD</td>
<td><p>FEaxisZAccel_fs-2</p>
<p>FEaxisZAccel_ms-2 (FEaxis_z_accel_fs-2)</p>
<p>or</p>
<p>GEaxisZAccel_fs-2</p>
<p>GEaxisZAccel_ms-2 (GEaxis_z_accel_fs-2)</p></td>
<td><p>Down Acceleration Toward Earth surface or center</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>76</td>
<td></td>
<td>AX</td>
<td><p>bodyXCgAccel_fs-2</p>
<p>bodyXCgAccel_ms-2 (body_x_cg_accel_fs-2)</p></td>
<td><p>X Acceleration Of A/c C.g. (body axis)</p>
<p>Includes the gravity vector.</p>
<p><mark>Is this actually body</mark>?</p></td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>77</td>
<td></td>
<td>AY</td>
<td><p>bodyYCgAccel_fs-2</p>
<p>bodyYCgAccel_ms-2 (body_y_cg_accel_fs-2)</p></td>
<td><p>Y Acceleration Of A/c C.g. (body axis)</p>
<p>Includes the gravity vector.</p></td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>78</td>
<td></td>
<td>AZ</td>
<td><p>bodyZCgAccel_fs-2</p>
<p>bodyZCgAccel_ms-2 (body_z_cg_accel_fs-2)</p></td>
<td><p>Z Acceleration Of A/c C.g. (body axis)</p>
<p>Includes the gravity vector.</p></td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>79</td>
<td></td>
<td>AXP</td>
<td>bodyXPilotAccel_fs-2 bodyXPilotAccel_ms-2
(body_x_pilot_accel_fs-2)</td>
<td>X Acceleration Of Pilot reference point (body axis)</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>80</td>
<td></td>
<td>AYP</td>
<td>bodyYPilotAccel_fs-2 bodyYPilotAccel_ms-2
(body_y_pilot_accel_fs-2)</td>
<td>Y Acceleration Of Pilot reference point(body axis)</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>81</td>
<td></td>
<td>AZP</td>
<td>bodyZPilotAccel_fs-2 bodyZPilotAccel_ms-2
(body_z_pilot_accel_fs-2)</td>
<td>Z Acceleration Of Pilot reference point(body axis)</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>82</td>
<td></td>
<td>G</td>
<td><p>localGravity_fs-2</p>
<p>localGravity_fs-2</p>
<p>(local_gravity_fs-2)</p></td>
<td>Acceleration Due To Gravity (at the vehicle altitude)</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>83</td>
<td>V<sub>CAL</sub></td>
<td>VCAL</td>
<td><p>calibratedAirspeed_nmih-1</p>
<p>(calibrated_airspeed_nmih-1)</p></td>
<td>Calibrated Air Speed, knots</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>95</td>
<td>I<sub>xx</sub></td>
<td>XIXX</td>
<td><p>bodyXXMomentOfInertia_slugf2</p>
<p>bodyXXMomentOfInertia_kgm2</p>
<p>(body_xx_moment_of_inertia_slugf2)</p></td>
<td><p>Vehicle X - Moment Of Inertia about Cg</p>
<p>body frame</p></td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.5.2</td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>96</td>
<td>I<sub>yy</sub></td>
<td>XIYY</td>
<td><p>bodyYYMomentOfInertia_slugf2</p>
<p>bodyYYMomentOfInertia_kgm2</p>
<p>(body_yy_moment_of_inertia_slugf2)</p></td>
<td><p>Vehicle Y - Moment Of Inertia about Cg</p>
<p>body frame</p></td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.5.2</td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>97</td>
<td>I<sub>zz</sub></td>
<td>XIZZ</td>
<td><p>bodyZZMomentOfInertia_slugf2</p>
<p>bodyZZMomentOfInertia_kgm2</p>
<p>(body_zz_moment_of_inertia_slugf2)</p></td>
<td><p>Vehicle Z - Moment Of Inertia about Cg</p>
<p>body frame</p></td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.5.2</td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>98</td>
<td>I<sub>xz</sub></td>
<td>XIXZ</td>
<td><p>bodyXZProductOfInertia_slugf2</p>
<p>bodyXZProductOfInertia_kgm2</p>
<p>(body_xz_product_of_inertia_slugf2)</p></td>
<td><p>Vehicle Xz Prod Of Inertia about Cg</p>
<p>body frame</p></td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.5.3</td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>99</td>
<td>I<sub>xy</sub></td>
<td>XIXY</td>
<td><p>bodyXYProductOfInertia_slugf2</p>
<p>bodyXYProductOfInertia_kgm2</p>
<p>(body_xy_product_of_inertia_slugf2)</p></td>
<td><p>Vehicle Xy Prod Of Inertia about Cg</p>
<p>body frame</p></td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.5.3</td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>100</td>
<td>I<sub>yz</sub></td>
<td>XIYZ</td>
<td><p>bodyYZProductOfInertia_slugf2</p>
<p>bodyYZProductOfInertia_kgm2</p>
<p>(body_yz_product_of_inertia_slugf2)</p></td>
<td><p>Vehicle Yz Prod Of Inertia about Cg</p>
<p>body frame</p></td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.5.3</td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>101</td>
<td>M</td>
<td>XMASS</td>
<td><p>totalMass_slug</p>
<p>totalMass_kg</p>
<p>(total_mass_slug)</p></td>
<td>Total Mass Of Vehicle (including Fuel, crew, cargo, stores,
passengers, etc.)</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>102</td>
<td>C<sub>L</sub></td>
<td>CL</td>
<td>coefficientOfLift (coefficient_of_lift)</td>
<td>Coefficient Of Lift, Total, includes effects of stores</td>
<td>UP</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td>103</td>
<td>C<sub>D</sub></td>
<td>CD</td>
<td>coefficientOfDrag (coefficient_of_drag)</td>
<td>Coefficient Of Drag, Total, includes effects of stores</td>
<td>AFT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>104</td>
<td>C<sub>X</sub></td>
<td>CX</td>
<td><p>aeroBodyXForceCoefficient</p>
<p>(aero_body_x_force_coefficient)</p></td>
<td>X-body Force Coefficient due to aerodynamic loads, includes stores
(Body axis)</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.6.3</td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td>105</td>
<td>C<sub>Y</sub></td>
<td>CY</td>
<td><p>aeroBodyYForceCoefficient</p>
<p>(aero_body_y_force_coefficient)</p></td>
<td>Y-body Force Coefficient due to aerodynamic loads, includes stores
(Body axis)</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.6.3</td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td>106</td>
<td>C<sub>Z</sub></td>
<td>CZ</td>
<td><p>aeroBodyZForceCoefficient</p>
<p>(aero_body_z_force_coefficient)</p></td>
<td>Z-body Force Coefficient due to aerodynamic loads, includes stores
(Body axis)</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td>10) 1.6.3</td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>107</td>
<td>F<sub>AX</sub></td>
<td>FAX</td>
<td><p>aeroBodyXForce_lbf</p>
<p>aeroBodyXForce_N</p>
<p>(aero_body_x_force_lbf)</p></td>
<td>Total X-body Force due to aerodynamic loads, includes stores (Body
axis)</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td>108</td>
<td>F<sub>AY</sub></td>
<td>FAY</td>
<td><p>aeroBodyYForce_lbf</p>
<p>aeroBodyYForce_N</p>
<p>(aero_body_y_force_N)</p></td>
<td>Total Y-body Force due to aerodynamic loads, includes stores (Body
axis)</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td>109</td>
<td>F<sub>AZ</sub></td>
<td>FAZ</td>
<td><p>aeroBodyZForce_lbf</p>
<p>aeroBodyZForce_N</p>
<p>(aero_body_z_force_lbf)</p></td>
<td>Total Z-body Force due to aerodynamic loads, includes stores (Body
axis)</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>110</td>
<td>F<sub>TX</sub></td>
<td><p>FEX</p>
<p>FTX</p></td>
<td><p>thrustBodyXForce_lbf</p>
<p>thrustBodyXForce_N</p>
<p>(thrust_body_x_force_lbf)</p></td>
<td>Total engine thrust Force, X-body axis</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td>111</td>
<td>F<sub>TY</sub></td>
<td><p>FEY</p>
<p>FTY</p></td>
<td><p>thrustBodyYForce_lbf</p>
<p>thrustBodyYForce_N</p>
<p>(thrust_body_y_force_lbf)</p></td>
<td>Total engine thrust Force, Y-body axis</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td>112</td>
<td>F<sub>TZ</sub></td>
<td><p>FEZ</p>
<p>FTZ</p></td>
<td><p>thrustBodyZForce_lbf</p>
<p>thrustBodyZForce_N</p>
<p>(thrust_body_z_force_lbf)</p></td>
<td>Total engine thrust Force, Z-body axis</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>113</td>
<td>F<sub>GX</sub></td>
<td>FGX</td>
<td><p>gearBodyXForce_lbf</p>
<p>gearBodyXForce_N</p>
<p>(gear_body_x_force_lbf)</p></td>
<td>Total landing gear Force, X-body axis</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td>114</td>
<td>F<sub>GY</sub></td>
<td>FGY</td>
<td><p>gearBodyYForce_lbf</p>
<p>gearBodyYForce_N</p>
<p>(gear_body_y_force_lbf)</p></td>
<td>Total landing gear Force, Y-body axis</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td>115</td>
<td>F<sub>GZ</sub></td>
<td>FGZ</td>
<td><p>gearBodyZForce_lbf</p>
<p>gearBodyZForce_N</p>
<p>(gear_body_z_force)</p></td>
<td>Total landing gear Force, Z-body axis</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>116</td>
<td>F<sub>x</sub></td>
<td><p>FTX</p>
<p>FX</p></td>
<td><p>totalBodyXForce_lbf</p>
<p>totalBodyXForce_N</p>
<p>(total_body_x_force_lbf)</p></td>
<td>Total Forces On A/c, X-body axis</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td>117</td>
<td>F<sub>y</sub></td>
<td><p>FTY</p>
<p>FY</p></td>
<td><p>totalBodyYForce_lbf</p>
<p>totalBodyYForce_N</p>
<p>(total_body_y_force_lbf)</p></td>
<td>Total Forces On A/c, Y-body axis</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td>118</td>
<td>F<sub>z</sub></td>
<td><p>FTZ</p>
<p>FZ</p></td>
<td><p>totalBodyZForce_lbf</p>
<p>totalBodyZForce_N</p>
<p>(total_body_z_force_lbf)</p></td>
<td>Total Forces On A/c, Z-body axis</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td><mark></mark></td>
<td><mark></mark></td>
<td><mark></mark></td>
<td><mark></mark></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>123</td>
<td>C<sub>l</sub></td>
<td>CLL</td>
<td>aeroBodyRollMomentCoefficient
(aero_body_roll_moment_coefficient)</td>
<td>Total Aerodynamic Rolling Moment Coeffocoent, Moment about the
X-body axis</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="odd">
<td>124</td>
<td>C<sub>m</sub></td>
<td>CLM</td>
<td>aeroBodyPitchMomentCoefficient
(aero_body_pitch_moment_coefficient)</td>
<td>Total Aerodynamic Pitching Moment Coeffocoent, Moment about the
Y-body axis</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td>3</td>
<td></td>
</tr>
<tr class="even">
<td><mark>125</mark></td>
<td><mark>C<sub>n</sub></mark></td>
<td><mark>CLN</mark></td>
<td><p><mark>aeroBodyYawMomentCoefficient
(aero_body_yaw_moment_coefficient)</mark></p>
<p><mark></mark></p></td>
<td><mark>Total Aerodynamic yawing Moment Coeffocoent, Moment about the
Z-body axis</mark></td>
<td><mark>ANR</mark></td>
<td><mark></mark></td>
<td><mark></mark></td>
<td><mark></mark></td>
<td><mark></mark></td>
<td><mark>3</mark></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>126</td>
<td>L<sub>A</sub></td>
<td>TAL</td>
<td><p>aeroBodyRollMoment_flbf aeroBodyRollMoment_Nm</p>
<p>(aero_body_roll_moment_flbf)</p></td>
<td>Total Aerodynamic Rolling moment (including attached stores), about
the X-body axis</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>127</td>
<td>M<sub>A</sub></td>
<td>TAM</td>
<td><p>aeroBodyPitchMoment_flbf aeroBodyPitchMoment_Nm</p>
<p>(aero_body_pitch_moment_flbf)</p></td>
<td>Total Aerodynamic pitching moment (including attached stores), about
the Y-body axis</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>128</td>
<td>N<sub>A</sub></td>
<td>TAN</td>
<td><p>aeroBodyYawMoment_flbf aeroBodyYawMoment_Nm</p>
<p>(aero_body_yaw_moment_flbf)</p></td>
<td>Total Aerodynamic yawing moment (including attached stores), about
the Z-body axis</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>129</td>
<td>L<sub>T</sub></td>
<td>TEL</td>
<td><p>thrustBodyRollMoment_flbf thrustBodyRollMoment_Nm</p>
<p>(thrust_body_roll_moment_flbf)</p></td>
<td>Total Engine Rolling Moment, about the X-body axis</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>130</td>
<td>L<sub>M</sub></td>
<td>TEM</td>
<td><p>thrustBodyPitchMoment_flbf thrustBodyPitchMoment_Nm</p>
<p>(thrust_body_pitch_moment_flbf)</p></td>
<td>Total Engine pitching Moment, about the Y-body axis</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td><mark>131</mark></td>
<td><mark>L<sub>N</sub></mark></td>
<td><mark>TEN</mark></td>
<td><p><mark>thrustBodyYawMoment_flbf thrustBodyYawMoment_Nm</mark></p>
<p><mark>(thrust_body_yaw_moment_flbf)</mark></p>
<p><mark></mark></p></td>
<td><p><mark>Total Engine yawing Moment, about the X-body
axis</mark></p>
<p><mark></mark></p></td>
<td><mark>ANR</mark></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>132</td>
<td>M<sub>gx</sub></td>
<td>TGL</td>
<td>landingGearBodyRollMoment_flbf landingGearBodyRollMoment_Nm
(landing_gear_body_roll_moment_flbf)</td>
<td>Total Landing Gear Rolling Moment, about the X-body axis</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>133</td>
<td>M<sub>gy</sub></td>
<td>TGM</td>
<td>landingGearBodyPitchMoment_flbf landingGearBodyPitchMoment_Nm
(landing_gear_body_pitch_moment_flbf)</td>
<td>Total Landing gear Pitch Moment, about the Y-body axis</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>134</td>
<td>M<sub>gz</sub></td>
<td>TGN</td>
<td>landingGearBodyYawMoment_flbf landingGearBodyYawMoment_Nm
(landing_g<mark>ear</mark>_body<mark>_yaw_moment_fl</mark>bf)</td>
<td>Total Landing Gear Yawing Moment, about the Z-body axis</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>135</td>
<td>Mtotx</td>
<td>TTL</td>
<td><p>totalBodyRollMoment_flbf</p>
<p>totalBodyRollMoment_Nm</p>
<p>(total_body_roll_moment_flbf)</p></td>
<td>Total Rolling Moment, about the X-body axis</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>136</td>
<td>Mtoty</td>
<td>TTM</td>
<td><p>totalBodyPitchMoment_flbf</p>
<p>totalBodyPitchMoment_Nm</p>
<p>(total_body_pitching_moment_flbf)</p></td>
<td>Total Pitching Moment, about the Y-body axis</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>137</td>
<td>Mtotz</td>
<td>TTN</td>
<td><p>totalBodyYawMoment_flbf</p>
<p>t<mark>otalBodyYawMoment_Nm</mark></p>
<p><mark>(total_body_yaw_moment_flbf)</mark></p></td>
<td>Total Yawing Moment, about the Z-body axis</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>138</td>
<td></td>
<td>HGT_RWY</td>
<td><p>run<mark>wayHeightAboveSL_ft</mark></p>
<p><mark>runwayHeightAboveSL_m</mark></p>
<p><mark>(runway_heig</mark>ht_above_SL_ft)</p></td>
<td>Height Of Runway W/r/t Sea Level</td>
<td>Above</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>139</td>
<td></td>
<td>XPLT2CG</td>
<td><p>pilotEyeBodyXCGReference_ft</p>
<p>pilotEyeBodyXCGReference_m</p>
<p>(pilot_eye_body_X_CG_reference_ft)</p></td>
<td>X Position Of Pilot eye point W/r/t C.g., in the body axis
system</td>
<td>Eye FWD of CG</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>140</td>
<td></td>
<td>YPLT2CG</td>
<td><p>pilotEyeBodyYCGReference_ft</p>
<p>pilotEyeBodyYCGReference_m</p>
<p>(pilot_eye_body_Y_CG_reference_ft)</p></td>
<td>Y Position Of Pilot eye point W/r/t C.g. , in the body axis
system</td>
<td>EyeRT of the CG</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>141</td>
<td></td>
<td>ZPLT2CG</td>
<td><p>pil<mark>otEyeBodyZCGReference_ft</mark></p>
<p><mark>pilotEyeBodyZCGReference_m</mark></p>
<p><mark>(pilot_eye_body_Z_CG_reference_f</mark>t)</p></td>
<td>Z Position Of Pilot eye point W/r/t C.g. , in the body axis
system</td>
<td>Eye below CG</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector of Geocentric Earth (GE) Fixed axis translational velocities
comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>142</td>
<td></td>
<td>XCG</td>
<td><p>GEaxisXTouchdownPoint_ft</p>
<p>GEaxisXTouchdownPoint_m</p>
<p>(GEaxis_X_touchdown_point_ft)</p>
<p>or</p>
<p>FEaxisXTouchdownPoint_ft</p>
<p>FEaxisXTouchdownPoint_m</p>
<p>(FEaxis_X_touchdown_point_ft)</p></td>
<td><p>C.g. X-position W/r/t Runway touchdown point</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>CG NORTH of TD point</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>143</td>
<td></td>
<td>YCG</td>
<td><p>GEaxisYTouchdownPoint_ft</p>
<p>GEaxisYTouchdownPoint_m</p>
<p>(GEaxis_Y_touchdown_point_ft)</p>
<p>or</p>
<p>FEaxisYTouchdownPoint_ft</p>
<p>FEaxisYTouchdownPoint_m</p>
<p>(FEaxis_Y_touchdown_point_ft)</p></td>
<td><p>C.g. Y-position W/r/t Runway</p>
<p>FE (flat earth or local) frame or GE frame, whichever
applies.</p></td>
<td>CG East of TD point</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td><mark>144</mark></td>
<td><mark></mark></td>
<td><mark>HCG</mark></td>
<td><p><mark>GEaxisZTouchdownPoint_ft</mark></p>
<p><mark>GEaxisZTouchdownPoint_m</mark></p>
<p><mark>(GEaxis_Z_touchdown_point_ft)</mark></p>
<p><mark>or</mark></p>
<p><mark>FEaxisZTouchdownPoint_ft</mark></p>
<p><mark>FEaxisZTouchdownPoint_m</mark></p>
<p><mark>(FEaxis_Z_touchdown_point_ft)</mark></p></td>
<td><p><mark>C.g. Z-position W/r/t Runway</mark></p>
<p><mark></mark></p>
<p><mark>FE (flat earth or local) frame or GE frame, whichever
applies.</mark></p>
<p><mark></mark></p>
<p><mark>(this variable is normally negative)</mark></p></td>
<td>CG below the TD point</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>145</td>
<td></td>
<td>WEIGHT</td>
<td><p>grossWeight_lbm</p>
<p>grossWeight_kg</p>
<p>(gross_weight_lbm)</p></td>
<td>Aircraft Gross Weight</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>146</td>
<td><mark>q</mark></td>
<td>QBAR</td>
<td>dynamicPressure_lbff-2 dynamicPressure_Nm-2 (dynamic_pressure_lbff-2
)</td>
<td>Dynamic Pressure</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>147</td>
<td><mark></mark><span
class="math inline">$\overline{q}$</span><mark><sub>c</sub></mark></td>
<td>QBARC</td>
<td>impactPressure_lbff-2 impactPressure_Nm-2 (impact_pressure_lbff-2
)</td>
<td>Inpact Pressure</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>148</td>
<td>A</td>
<td>AREA</td>
<td><p>referenceWingArea_f2</p>
<p>referenceWingArea_m2</p>
<p>(reference_wing_area_f2)</p></td>
<td>Reference Wing Area</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>149</td>
<td>b</td>
<td>SPAN</td>
<td><p>referenceWingSpan_f</p>
<p>referenceWingSpan_m</p>
<p>(reference_wing_span_f)</p></td>
<td>Reference Wing Span</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>150</td>
<td>c</td>
<td>CHORD</td>
<td><p>referenceWingChord_f</p>
<p>referenceWingChord_m</p>
<p>(reference_wing_chord_f)</p></td>
<td>Mean Aerodynamic Chord (reference wing chord)</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>151</td>
<td>ρ</td>
<td>RHO</td>
<td><p>airDensity_lbmf-3</p>
<p>airDensity_kgpm-3</p>
<p>(air_density_lbmf-3 )</p></td>
<td>Air Density, At Altitude</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>152</td>
<td>a</td>
<td>SOUND</td>
<td><p>speedOfSound_fs-2</p>
<p>speedOfSound_ms-2</p>
<p>(speed_of_sound_fs-2)</p></td>
<td>Velocity Of Sound At Altitude</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td><p>eulerAngleInitialCondition_d(3)</p>
<p>eulerAngleInitialCondition_r(3)</p>
<p>(euler_angle_initial_condition_d(3))</p></td>
<td>Vector of initial Euler angles comprised of the three components as
defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>153</td>
<td></td>
<td>PHIIC</td>
<td><p>rollEulerAngleInitialCondition_d</p>
<p>rollEulerAngleInitialCondition_r</p>
<p>(roll_euler_angle_initial_condition_d)</p></td>
<td>Initial Roll Angle</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>154</td>
<td></td>
<td>THETIC</td>
<td><p>pitchEulerAngleInitialCondition_d</p>
<p>pitchEulerAngleInitialCondition_r</p>
<p>(pitch_euler_angle_initial_condition_d)</p></td>
<td>Initial Pitch Angle</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>155</td>
<td></td>
<td>PSIIC</td>
<td><p>yawEulerAngleInitialCondition_d</p>
<p>yawEulerAngleInitialCondition_r</p>
<p>(yaw_euler_angle_initial_condition_d)</p></td>
<td>Initial Yaw Angle</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>156</td>
<td>γ<sub>VIC</sub></td>
<td>GAMVIC</td>
<td><p>flightPathAngleInitialCondition_r</p>
<p>flightPathAngleInitialCondition_d</p>
<p>(flight_path_angle_ initial_condition_r)</p></td>
<td>Initial Vertical Flt Path Angle</td>
<td>AH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>157</td>
<td>Γ<sub>HIC</sub></td>
<td>GAMHIC</td>
<td><p>flightPathAzimuthInitialCondition_r</p>
<p>flightPathAzimuthInitialCondition_d</p>
<p>(flight_path_azimuth_ initial_condition_r)</p>
<p><mark>(Ground_Track_Velocity_Angle)</mark></p></td>
<td>Initial Horizontal Flt Path Angle</td>
<td>CWFN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td><p>s_bodyAngulerRateInitialCondition_rs-1(3)</p>
<p>s_bodyAngularRateInitialCondition_ds-1(3) (s_body_anguler_rate_
initial_condition_rs-1(3))</p></td>
<td>Vector of initial body axis anguler rates comprised of the three
components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>158</td>
<td></td>
<td>PBIC</td>
<td>s_bodyRollRateInitialCondition_rs-1
s_bodyRollRateInitialCondition_ds-1 (s_body_roll_rate_
initial_condition_rs-1)</td>
<td>Initial Roll Angular Rate</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>159</td>
<td></td>
<td>QBIC</td>
<td>s_bodyPitchRateInitialCondition_rs-1
s_bodyPitchRateInitialCondition_ds-1 (s_body_pitch_rate_
initial_condition_rs-1)</td>
<td>Initial Pitch Angular Rate</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>160</td>
<td></td>
<td>RBIC</td>
<td>s_bodyYawRateInitialCondition_rs-1
s_bodyYawRateInitialCondition_ds-1 (s_body_yaw_rate_
initial_condition_rs-1)</td>
<td>Initial Yaw Angular Rate</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>161</td>
<td></td>
<td><mark>VEQIC</mark></td>
<td>equivalentAirspeedInitialCondition_nmih-1</td>
<td>Initial Equiv Air Speed</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>162</td>
<td></td>
<td>XCG</td>
<td><p>GEaxisXTouchdownPointInitialCondition_ft</p>
<p>GEaxisXTouchdownPointInitialCondition_m</p>
<p>(GEaxis_X_touchdown_point<mark>_initial_condition</mark>_ft)</p>
<p>or</p>
<p>FEaxisXTouchdownPointInitialCondition_ft</p>
<p>FEaxisXTouchdownPointInitialCondition_m</p>
<p>(FEaxis_X_touchdown_point<mark>_initial_condition</mark>_ft)</p></td>
<td>Initial Distance From Runway</td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>163</td>
<td></td>
<td>YCG</td>
<td><p>GEaxisYTouchdownPointInitialCondition_ft</p>
<p>GEaxisYTouchdownPointInitialCondition_m</p>
<p>(GEaxis_Y_touchdown_point<mark>_initial_condition</mark>_ft)</p>
<p>or</p>
<p>FEaxisYTouchdownPointInitialCondition_ft</p>
<p>FEaxisYTouchdownPointInitialCondition_m</p>
<p>(FEaxis_Y_touchdown_point<mark>_initial_condition</mark>_ft)</p></td>
<td>Initial Distance From Runway</td>
<td>EAST</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>164</td>
<td></td>
<td><mark>HCG</mark></td>
<td><p><mark>GEaxisZTouchdownPoint</mark>InitialCondition<mark>_ft</mark></p>
<p><mark>GEaxisZTouchdownPoint</mark>InitialCondition<mark>_m</mark></p>
<p><mark>(GEaxis_Z_touchdown_point_initial_condition_ft)</mark></p>
<p><mark>or</mark></p>
<p><mark>FEaxisZTouchdownPoint</mark>InitialCondition<mark>_ft</mark></p>
<p><mark>FEaxisZTouchdownPoint</mark>InitialCondition<mark>_m</mark></p>
<p><mark>(FEaxis_Z_touchdown_point_initial_condition_ft)</mark></p></td>
<td>Initial Height Above Sea Level</td>
<td>UP</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>165</td>
<td></td>
<td>WEIGHTIC</td>
<td><p>grossWeightInitialCondition_lbm</p>
<p>grossWeightInitialCondition_kg</p>
<p>(gross_weight_initial_condition_lbm)</p></td>
<td>Initial Gross Weight</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>166</td>
<td></td>
<td>CG</td>
<td><p>XBodyCGReference_f</p>
<p>XBodyCGReference_m</p>
<p>(X_body_CG_reference_f)</p></td>
<td>C.g. Position W/r/t L.e. Of the mean aerodynamic chord</td>
<td>AFT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>167</td>
<td>a<sub>SL</sub></td>
<td>SOUND_SL</td>
<td><p>seaLevelSpeedOfSound_fs-2</p>
<p>seaLevelSpeedOfSound_ms-2</p>
<p>(sea_level_speed_of_sound_fs-2)</p></td>
<td>Standard day speed of sound @ sea level</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>168</td>
<td></td>
<td>TIME</td>
<td><p>simTime_s</p>
<p>simTime_s</p>
<p>(sim_time_s)</p></td>
<td>Time Since Start Of Operate Mode</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>169</td>
<td></td>
<td>TR</td>
<td><p>totalTempRatio_C</p>
<p>totalTempRatio_K</p>
<p>(total_temp_ratio_C)</p></td>
<td>Total Temperature Ratio</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>170</td>
<td></td>
<td>PR</td>
<td><p>totalPressureRatio_C</p>
<p>totalPressureRatio_K</p>
<p>(total_pressure_ratio_C)</p></td>
<td>Total Pressure Ratio</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>171</td>
<td></td>
<td>D2R</td>
<td><p>degToRad</p>
<p>degToRad</p>
<p>(deg_to_rad)</p></td>
<td>0.01745329 Deg To Rad Conversion Factor</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>172</td>
<td></td>
<td>R2D</td>
<td><p>radToDeg</p>
<p>radToDeg</p>
<p>(rad_to_d)</p></td>
<td>57.2957795 Rad To Deg Conversion Factor</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>173</td>
<td>T<sub>AMB</sub></td>
<td>TAMB</td>
<td><p>ambientTemperature_C</p>
<p>ambientTemperature_K</p>
<p>(ambient_temperature_C)</p></td>
<td>Ambient Temperature at altitude</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>174</td>
<td>P<sub>AMB</sub></td>
<td>PAMB</td>
<td><p>ambientPressure_lbff-2</p>
<p>ambientPressure_Nm-2</p>
<p>(ambient_pressure_lbff-2)</p></td>
<td>Ambient Pressure at altitude</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>175</td>
<td>T<sub>TOT</sub></td>
<td>TTOT</td>
<td><p>totalTemp_C</p>
<p>totalTemp_K</p>
<p>(total_temp_C)</p></td>
<td>Total Temperature at altitude</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>176</td>
<td>P<sub>TOT</sub></td>
<td>PTOT</td>
<td><p>totalPressure_lbff-2</p>
<p>totalPressure_Nm-2</p>
<p>(total_pressure_lbff-2)</p></td>
<td>Total Pressure at altitude</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>177</td>
<td>I<sub>EXX</sub></td>
<td>IEXX</td>
<td><p>engineXXMomentOfInertia_slugf2</p>
<p>engineXXMomentOfInertia_kgm2</p>
<p>(engine_xx_moment_of_inertia_slugf2)</p></td>
<td><p>Moment of inertia about the X-axis Of Rotating Eng, for an engine
with the propeller, includes the propeller</p>
<p>This is wrt the axis of the engine</p></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>178</td>
<td>I<sub>EYY</sub></td>
<td>IEYY</td>
<td><p>engineYYMomentOfInertia_slugf2</p>
<p>engineYYMomentOfInertia_kgm2</p>
<p>(engine_yy_moment_of_inertia_slugf2)</p></td>
<td><p>Moment of inertia about the Y-axis Of Rotating Eng, for an engine
with the propeller, includes the propeller</p>
<p>This is wrt the axis of the engine</p></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>179</td>
<td>I<sub>EZZ</sub></td>
<td>IEZZ</td>
<td><p>engineZZMomentOfInertia_slugf2</p>
<p>engineZZMomentOfInertia_kgm2</p>
<p>(engine_zz_moment_of_inertia_slugf2)</p></td>
<td><p>Moment of inertia about the Z-axis Of Rotating Eng, for an engine
with the propeller, includes the propeller</p>
<p>This is wrt the axis of the engine</p></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td>I<sub>EXZ</sub></td>
<td>IEXZ</td>
<td><p>engineXZProductOfInertia_slugf2</p>
<p>engineXZProductOfInertia_kgm2</p>
<p>(engine_xz_product_of_inertia_slugf2)</p></td>
<td><p>Product of inertia about the XZ-axis Of Rotating Eng, for an
engine with the propeller, includes the propeller</p>
<p>This is wrt the axis of the engine</p></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td>I<sub>EXY</sub></td>
<td>IEXY</td>
<td><p>engineXYProductOfInertia_slugf2</p>
<p>engineXYProductOfInertia_kgm2</p>
<p>(engine_xy_product_of_inertia_slugf2)</p></td>
<td><p>Product of inertia about the XY-axis Of Rotating Eng, for an
engine with the propeller, includes the propeller</p>
<p>This is wrt the axis of the engine</p></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td>I<sub>EYZ</sub></td>
<td>IEYZ</td>
<td><p>engineYZProductOfInertia_slugf2</p>
<p>engineYZProductOfInertia_kgm2</p>
<p>(engine_yz_product_of_inertia_slugf2)</p></td>
<td><p>Product of inertia about the YZ-axis Of Rotating Eng, for an
engine with the propeller, includes the propeller</p>
<p>This is wrt the axis of the engine</p></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector _________________ comprised of the three components as
defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>180</td>
<td>u<sub>B</sub></td>
<td>UBD or sd_UBD</td>
<td><p>sd_bodyXacceleration_fs-2</p>
<p>sd_bodyXacceleration_ms-2</p>
<p>(sd_body_X_acceleration_fs-2)</p></td>
<td><p>Lnongitudinal acceleration (along the X-body axis)</p>
<p><mark>EOM can be formulated such that UBD is not a state derivative,
correct?</mark></p></td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>181</td>
<td>v<sub>B</sub></td>
<td>VBD or sd_VBD</td>
<td><p>sd_bodyYacceleration_fs-2</p>
<p>sd_bodyYacceleration_ms-2</p>
<p>(sd_body_Y_acceleration_fs-2)</p></td>
<td>Right Sideward Acceleration, B-axis</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>182</td>
<td>w<sub>B</sub></td>
<td>WBD or sd_WBD</td>
<td><p>sd_bodyZacceleration_fs-2</p>
<p>sd_bodyZacceleration_ms-2</p>
<p>(sd_body_Z_acceleration_fs-2)</p></td>
<td>Downward Acceleration, B-axis</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector _________________ comprised of the three components as
defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>183</td>
<td></td>
<td>VTWN</td>
<td><p>netWindVelFromNorth_fs-1</p>
<p>netWindVelFromNorth_ms-1</p>
<p>(net_wind_vel_from_north_fs-1)</p></td>
<td><p>Net wind velocity from north</p>
<p>(plus means wind is coming from the North)</p>
<p>Net wind is the steady state winds plus any turbulences and
shears.</p></td>
<td>NORTH (plus means wind</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>184</td>
<td></td>
<td>VTWE</td>
<td><p>netWindVelFromEast_fs-1</p>
<p>netWindVelFromEast_ms-1</p>
<p>(net_wind_vel_from_east_fs-1)</p></td>
<td><p>Net wind velocity from East (plus means wind is coming from the
East)</p>
<p>Net wind is the steady state winds plus any turbulences and
shears.</p></td>
<td>EAST</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>185</td>
<td></td>
<td>VTWD</td>
<td><p>netWindVelFromBelow_fs-1</p>
<p>netWindVelFromBelow_ms-1</p>
<p>(net_wind_vel_from_below_fs-1)</p></td>
<td><p>Net wind velocity from below (plus means wind is coming from
below)</p>
<p>Net wind is the steady state winds plus any turbulences and
shears.</p></td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector _________________ comprised of the three components as
defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>186</td>
<td></td>
<td>VNTURB</td>
<td>turbulenceFromNorth_fs-1 turbulenceFromNorth_ms-1
(turbulence_from_north_fs-1)</td>
<td>North component of turbulence (plus means turbulence is coming from
the North)</td>
<td>NORTH</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>187</td>
<td></td>
<td>VETURB</td>
<td>turbulenceFromEast_fs-1 turbulenceFromEast_ms-1
(turbulence_from_east_fs-1)</td>
<td>East component of turbulence (plus means turbulence is coming from
the East)</td>
<td>EAST</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>188</td>
<td></td>
<td>VDTURB</td>
<td>turbulenceFromBelow_fs-1 turbulenceFromBelow_ms-1
(turbulence_from_below_fs-1)</td>
<td>Down component of turbulence (plus means turbulence is coming from
below)</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>189</td>
<td></td>
<td>PAMBR</td>
<td><p>ambientPressureRatio</p>
<p>(Ambient_Pressure_Ratio)</p></td>
<td><mark>Ratio Of ambient pressure at altitude to sea level ambient
ressure</mark></td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>190</td>
<td></td>
<td>TAMBR</td>
<td><p>ambientTemperatureRatio</p>
<p>(ambient_temperature_ratio)</p></td>
<td><mark>Ratio Of ambient temperature at altitude to sea level ambient
temp.</mark></td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector _________________ comprised of the three components as
defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>191</td>
<td>∆X<sub>cg</sub></td>
<td>DXCG</td>
<td><p>aircraftBodyXCGPosition_ft</p>
<p>aircraftBodyXCGPosition_m</p>
<p>(aircraft_body_X_CG_position_ft)</p></td>
<td>Cg Displacement From the aerodynamic force and moment reference
center, + is CG fwd of the Aerodynamcic Reference Center (ARC). The ARC
is the reference point that the aero model forces and moments act upon
the aircraft.</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>192</td>
<td>∆Y<sub>cg</sub></td>
<td>DYCG</td>
<td><p>aircraftBodyYCGPosition_ft</p>
<p>aircraftBodyYXCGPosition_m</p>
<p>(aircraft_body_Y_CG_position_ft)</p></td>
<td>Cg Displacement From the aerodynamic force and moment reference
center, + is CG to the right of the ARC</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>193</td>
<td>∆Z<sub>cg</sub></td>
<td><mark>DZCG</mark></td>
<td><p><mark>aircraftBodyZCGPosition_ft</mark></p>
<p><mark>aircraftBodyZCGPosition_m</mark></p>
<p><mark>(aircraft_body_Z_CG_position_ft)</mark></p></td>
<td><mark>Cg Displacement From the aerodynamic force and moment
reference center, + is CG below the the ARC</mark></td>
<td>DWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>194</td>
<td>p<sub>s</sub></td>
<td>PS</td>
<td>stabilityaxisRollRate_rs-1 stabilityaxisRollRate_ds-1
(stabilityaxis_roll_rate_rs-1)</td>
<td><p>Stability Axis roll rate</p>
<p><mark>Haven’t defined stability axis</mark></p></td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>195</td>
<td>r<sub>s</sub></td>
<td>RS</td>
<td>stabilityaxisYawRate_rs-1 stabilityaxisYawRate_ds-1
(stabilityaxis_yaw_rate_rs-1)</td>
<td>Stability Axis yaw rate</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>196</td>
<td></td>
<td>PBDEG</td>
<td>Body_Roll_Acceleration_ds-2</td>
<td>Roll rate, body axis</td>
<td>RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>197</td>
<td></td>
<td>QBDEG</td>
<td>Body_Pitch_Acceleration_ds-2</td>
<td>Pitch rate, body axis</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>198</td>
<td></td>
<td>RBDEG</td>
<td>Body_Yaw_Acceleration_ds-2</td>
<td>Yaw rate, body axis</td>
<td>ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>199</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>200</td>
<td></td>
<td>IWEEL</td>
<td></td>
<td>Landing Gear Down</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>201</td>
<td></td>
<td>IWEELC</td>
<td></td>
<td>Command Landing Gear Down</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>202</td>
<td></td>
<td>ILGTRN</td>
<td></td>
<td>Landing Gear In Transit</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>203</td>
<td></td>
<td>IPARAC</td>
<td></td>
<td>Activate Parachute</td>
<td>NSC</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>204</td>
<td></td>
<td>IATCG</td>
<td></td>
<td>Cg Reference Point Moment Transfer FlagND</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>205</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>206</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>207</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>208</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>209</td>
<td></td>
<td>NX</td>
<td></td>
<td>X Body acceleration at CG, includes the gravity vector</td>
<td>FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>210</td>
<td></td>
<td>NY</td>
<td></td>
<td>Y Body acceleration at CG, includes the gravity vector</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>211</td>
<td></td>
<td>NZ</td>
<td></td>
<td>Z Body acceleration at CG, includes the gravity vector</td>
<td>DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>212</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>213</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>228</td>
<td></td>
<td>DTAMB_R</td>
<td></td>
<td>Delta to ambient temperature, deg Rankin</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>229</td>
<td></td>
<td>XCGLOC</td>
<td></td>
<td>X-location in inertial space of CG</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>230</td>
<td></td>
<td>YCGLOC</td>
<td></td>
<td>Y-location in inertial space of CG</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>231</td>
<td></td>
<td>ZCGLOC</td>
<td></td>
<td>Z-location in inertial space of CG</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector comprised of the three components as defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>232</td>
<td></td>
<td>XPLOC</td>
<td></td>
<td>X-location in inertial space of pilot</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>233</td>
<td></td>
<td>YPLOC</td>
<td></td>
<td>Y-location in inertial space of pilot</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>234</td>
<td></td>
<td>ZPLOC</td>
<td></td>
<td>Z-location in inertial space of pilot</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>235</td>
<td></td>
<td>RR</td>
<td></td>
<td>Radius of Earth + height of rwy above SL</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>236</td>
<td></td>
<td>UUU</td>
<td></td>
<td>Inertial velocity trans to body x-axis</td>
<td>+FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>237</td>
<td></td>
<td>VVV</td>
<td></td>
<td>Inertial velocity trans to body y-axis</td>
<td>+RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>238</td>
<td></td>
<td>WWW</td>
<td></td>
<td>Inertial velocity trans to body z-axis</td>
<td>+DWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector _________________ comprised of the three components as
defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>239</td>
<td></td>
<td>PTURB</td>
<td></td>
<td>Body axis roll turbulence</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>240</td>
<td></td>
<td>QTURB</td>
<td></td>
<td>Body axis pitch turbulence</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>241</td>
<td></td>
<td>RTURB</td>
<td></td>
<td>Body axis yaw turbulence</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td>Vector _________________ comprised of the three components as
defined below.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>242</td>
<td></td>
<td>PBWN</td>
<td></td>
<td>Roll rate wrt roll turbulence</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>243</td>
<td></td>
<td>QBWN</td>
<td></td>
<td>Pitch rate wrt pitch turbulence</td>
<td>UP</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>244</td>
<td></td>
<td>RBWN</td>
<td></td>
<td>Yaw rate wrt yaw turbulence</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>245</td>
<td></td>
<td>PSWN</td>
<td></td>
<td>Stability axis roll rate w/turb</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>246</td>
<td></td>
<td>RSWN</td>
<td></td>
<td>Stability axis yaw rate w/turb</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>247</td>
<td></td>
<td>RALT</td>
<td><p>heightAboveTerrain_f</p>
<p>heightAboveTerrain_m</p></td>
<td>height above the terrain</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>248</td>
<td></td>
<td>RE</td>
<td>Radius_of_Smooth_Earth_f</td>
<td>Radius of Earth (center to smooth surface which is mean sea level),
round earth model</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td>H_O_T</td>
<td><p>heightOfTerrain_f</p>
<p>heightOfTerrain_m</p>
<p>(Height_of_Terrain_f)</p></td>
<td>Height of the terrain under the a/c cg. It is the terrain height
above the smooth surface of of the earth, regardless whether a flat,
round or oblate spheroid model is used.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td>RE_OS</td>
<td>Radius_Of_Oblate_Spheroid_Earth_f</td>
<td>Radius of Earth, center to smooth surface, oblate spheroid earth
model.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>249</td>
<td></td>
<td>DTINV</td>
<td></td>
<td>Inverse of simulation time step</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>250</td>
<td></td>
<td>G_INV</td>
<td></td>
<td>Inverse of acceleration due to gravity</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>251</td>
<td></td>
<td>FPS2KTS</td>
<td></td>
<td>Conversion from feet/sec to knots</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>252</td>
<td></td>
<td>KTS2FPS</td>
<td></td>
<td>Conversion from knots to feet/sec</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>253</td>
<td></td>
<td>TAMB_R</td>
<td></td>
<td>Ambient temperature, degrees Rankin</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>254</td>
<td></td>
<td>TTOT_R</td>
<td></td>
<td>Total temperature, degrees Rankin</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>255</td>
<td></td>
<td>ALT_SET</td>
<td></td>
<td>Altimeter setting (Kohlsman window)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>256</td>
<td></td>
<td>ALT_PRESSURE</td>
<td>Pressure_Altitude_f</td>
<td>Pressure altitude</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>257</td>
<td></td>
<td>ALT_TAMB_REF</td>
<td></td>
<td>Altitude at reference temperature</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>258</td>
<td></td>
<td>TAMB_R_REF</td>
<td></td>
<td>Ref. ambient temperature (non-standard)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>259</td>
<td></td>
<td>RHO_SL</td>
<td>seaLevelAirDensity_lbfpf3</td>
<td>Air density at sea level</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>260</td>
<td></td>
<td>TAMB_R_SL</td>
<td>seaLevelAmbientTemp_</td>
<td>Standard day ambient temperature</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>261</td>
<td></td>
<td>PAMB_SL</td>
<td></td>
<td>Standard day ambient pressure</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>262</td>
<td></td>
<td>CGXREF</td>
<td>(X_CG_Reference_Inches_Constant)</td>
<td>X-location of reference CG (fuselage sta</td>
<td>AFT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>263</td>
<td></td>
<td>CGYREF</td>
<td>(Y_CG_Reference_Inches_Constant)</td>
<td>Y-location of reference CG (buttline)</td>
<td>LEFT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>264</td>
<td></td>
<td>CGZREF</td>
<td>(Z_CG_Reference_Inches_Constant)</td>
<td>Z-location of reference CG (waterline)</td>
<td>UP</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>265</td>
<td></td>
<td>PI</td>
<td>pi</td>
<td>Constant = pi = 3.14159</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>267</td>
<td></td>
<td>RALT_TERRAIN</td>
<td></td>
<td>Radar alt perpendicular to terrain slope</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>268</td>
<td></td>
<td>VNGUST</td>
<td></td>
<td>North wind gust component</td>
<td>North</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>269</td>
<td></td>
<td>VEGUST</td>
<td></td>
<td>East wind gust component</td>
<td>East</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>270</td>
<td></td>
<td>VDGUST</td>
<td></td>
<td>Down wind gust component</td>
<td>Down</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>271</td>
<td></td>
<td>WIND_SPEED</td>
<td></td>
<td>Total velocity of steady wind</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>272</td>
<td></td>
<td>WIND_DIRECTION</td>
<td></td>
<td>Steady wind heading (blowing FROM)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>273</td>
<td></td>
<td>UBURB</td>
<td></td>
<td>Body x-axis component of carrier burbleFT/S</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>274</td>
<td></td>
<td>VBURB</td>
<td></td>
<td>Body y-axis component of carrier burbleFT/S</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>275</td>
<td></td>
<td>WBURB</td>
<td></td>
<td>Body z-axis component of carrier burbleFT/S</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>276</td>
<td></td>
<td>PBURB</td>
<td></td>
<td>Roll component of carrier burble</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>277</td>
<td></td>
<td>QBURB</td>
<td></td>
<td>Pitch component of carrier burb</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>278</td>
<td></td>
<td>TURB_LEVEL</td>
<td></td>
<td>Level of severity of turbulence</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>279</td>
<td></td>
<td>TURB_MODEL</td>
<td></td>
<td>DRYDEN = 1, Von Karman = 2</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>280</td>
<td></td>
<td>TURB_TYPE</td>
<td></td>
<td>Random = 1, Repeatable = 2</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>281</td>
<td></td>
<td>GUST_LEVEL</td>
<td></td>
<td>Step gust level - magnitude,frequency</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>282</td>
<td></td>
<td>BURB_TYPE</td>
<td></td>
<td>Ship burble type 0-off,1-random,2:11 rpt</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>283</td>
<td></td>
<td>FDX</td>
<td></td>
<td>Delta to x-axis body force</td>
<td>+FWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>284</td>
<td></td>
<td>FDY</td>
<td></td>
<td>Delta to y-axis body force</td>
<td>+RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>285</td>
<td></td>
<td>FDZ</td>
<td></td>
<td>Delta to z-axis body force</td>
<td>+DOWN</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>286</td>
<td></td>
<td>TDL</td>
<td></td>
<td>Delta to roll moment</td>
<td>+RWD</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>287</td>
<td></td>
<td>TDM</td>
<td></td>
<td>Delta to pitch moment</td>
<td>+ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>288</td>
<td></td>
<td>TDN</td>
<td></td>
<td>Delta to yaw moment</td>
<td>+ANR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>289</td>
<td></td>
<td>IFLAPC</td>
<td></td>
<td>Flap command (0:retract, 1..n:extend)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>290</td>
<td></td>
<td>IFLAP</td>
<td></td>
<td>Flap status (-1:trans,0:up,1..n out)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>291</td>
<td></td>
<td>IWOW</td>
<td>(Weight_On_Wheels)</td>
<td>Weight-on-wheels flag (0:none,1:on)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>292</td>
<td></td>
<td>SLOPE_RWY</td>
<td></td>
<td>Slope (ie "pitch") of runway</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>293</td>
<td></td>
<td>BANK_RWY</td>
<td></td>
<td>Bank (ie "roll") of runway</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>294</td>
<td></td>
<td>CBNKRWY</td>
<td></td>
<td>Cosine of runway Euler bank angle</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>295</td>
<td></td>
<td>SBNKRWY</td>
<td></td>
<td>Sine of runway Euler bank angle</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>296</td>
<td></td>
<td>CSLPRWY</td>
<td></td>
<td>Cosine of runway Euler pitch angle</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>297</td>
<td></td>
<td>SSLPRWY</td>
<td></td>
<td>Sine of runway Euler pitch angle</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>298</td>
<td></td>
<td>PBGUST</td>
<td></td>
<td>Body axis roll gust</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>299</td>
<td></td>
<td>QBGUST</td>
<td></td>
<td>Body axis pitch gust</td>
<td>RT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>300</td>
<td></td>
<td>TAMB_C</td>
<td></td>
<td>Ambient temp.- used for non-standard day</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>301</td>
<td></td>
<td>ALT_DENSITY</td>
<td></td>
<td>Density altitude</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>302</td>
<td></td>
<td>PAMB_ST</td>
<td></td>
<td>Ambient pressure, standard day</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>303</td>
<td></td>
<td>TAMB_R_ST</td>
<td></td>
<td>Ambient temperature, standard day</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>304</td>
<td></td>
<td>RHO_ST</td>
<td></td>
<td>Ambient density, standard day</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>305</td>
<td></td>
<td>DELTA_PAMB</td>
<td></td>
<td>Ambient pressure delta from standard day</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>306</td>
<td></td>
<td>DELTA_TAMB</td>
<td></td>
<td>Ambient temp. delta from standard day</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>307</td>
<td></td>
<td>DELTA_RHO</td>
<td></td>
<td>Ambient density delta from standard daySLUG/FT3</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>308</td>
<td></td>
<td>NS_PAMB</td>
<td></td>
<td>Non-standard ambient pressure flag</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>309</td>
<td></td>
<td>NS_ALTP</td>
<td></td>
<td>Non-standard pressure altitude flag</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>310</td>
<td></td>
<td>NS_TAMB</td>
<td></td>
<td>Non-standard ambient temperature flag</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>311</td>
<td></td>
<td>NS_DENS</td>
<td></td>
<td>Non-standard ambient density flag</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>312</td>
<td></td>
<td>ALFA_TRIM</td>
<td></td>
<td>Target angle of attack for trim</td>
<td>ANU</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td>313</td>
<td></td>
<td>BETA_TRIM</td>
<td></td>
<td>Target angle of sideslip for trim</td>
<td>ANL</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Trailing_Edge_Flap_Deflection</td>
<td>Trailing edge flap deflection</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Leading_Edge_Flap_Deflection</td>
<td>Leading edge flap deflection</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Spoiler_Deflection</td>
<td>Spoiler deflection</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Aileron_Deflection</td>
<td>Aileron deflection</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Rudder_Deflection</td>
<td>Rudder deflection</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Stabilizer_Deflection</td>
<td>Stabilizer deflection</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Speedbrake_Deflection</td>
<td>Speedbrake deflection</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Canard_Deflection</td>
<td>Canard Deflection</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Elevator_Deflection</td>
<td>Elevator deflection</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Aircraft_Landing_Gear_Status_Position</td>
<td>array of gear positions (array)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Ownship_Linear_Velocity</td>
<td>Ownship linear velocity VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Ownship_Linear_Acceleration</td>
<td>Ownship linear acceleration VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Ownship_Angular_Position</td>
<td>Ownship angular position VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Ownship_Angular_Velocity</td>
<td>Ownship angular velocity VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Ownship_Angular_Acceleration</td>
<td>Ownship angular acceleration VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Ownship_Earth_Axis_Velocity</td>
<td>Ownship earth axis velocity VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Ownship_Earth_Axis_Acceleration</td>
<td>ownship earth axis acceleration VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Ownship_Attitude_Relative_To_Deck</td>
<td>Ownship attitude relative to deck VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Quaternion_E1</td>
<td>Quaternion E1</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Quaternion_E2</td>
<td>Quaternion E2</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Quaternion_E3</td>
<td>Quaternion E3</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Quaternion_E4</td>
<td>Quaternion E4</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Last_Times_Quaternion_E1_Rate</td>
<td>previous Quaternion E1 dot</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Last_Times_Quaternion_E2_Rate</td>
<td>previous Quaternion E2 dot</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Last_Times_Quaternion_E3_Rate</td>
<td>previous Quaternion E3 dot</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Last_Times_Quaternion_E4_Rate</td>
<td>previous Quaternion E4 dot</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Delta_Time</td>
<td>Time step</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Body_To_Earth_Transformation_Matrix</td>
<td>Transformation matrix from body axis to earth axis</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Direction_Cosine_Matrix</td>
<td>matrix of direction cosines</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Angle_Of_Attack_At_Stall_Onset</td>
<td>Angle of attack at stall onset</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Body_Air_Velocity</td>
<td>Body air velocity VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Body_Air_Acceleration</td>
<td>Body air acceleration VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Normal_Load_Factor</td>
<td>(Fxb*Sin(alpha)-Fzb*Cos(alphs))/Wgross</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Platform_Velocity</td>
<td>platform velocity VECTOR (see CRAFT_RA.A)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Air_Density_Ratio</td>
<td>Air density ratio (Rho_amb/Rho_std_SL)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Meridional_Earth_Radius</td>
<td>(see EAR_RAD.A)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Normal_Earth_Radius</td>
<td><p>round or oblate spheroid earth model?</p>
<p>(see EAR_RAD.A)</p></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Geodetic_Altitude</td>
<td>(see CRAFT_RA.A)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Wander_Angle</td>
<td>(see CRAFT_RA.A)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Earth_Rotation_X_Rate</td>
<td>Earth rotation x rate (see EAR_RO_R.A)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Earth_Rotation_Y_Rate</td>
<td>Earth rotation y rate (see EAR_RO_R.A)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Earth_Rotation_Z_Rate</td>
<td>Earth rotation z rate (see EAR_RO_R.A)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Coriolis_Acceleration</td>
<td>Coriolis acceleration VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Craft_X_Velocity</td>
<td>Craft x velocity (see CRAFT_RA.A)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Craft_Y_Velocity</td>
<td>Craft y velocity (see CRAFT_RA.A)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Fuel_Tank_Quantities</td>
<td>Array of fuel weights of each tank</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Drift_Angle</td>
<td>= (true heading) - (ground track)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>X_CG_Location</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Lift_Due_Do_Angle_Of_Attack</td>
<td>lift due to angle of attack</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Lift_Due_To_Angle_Of_Attack_Rate</td>
<td>Lift due to angle of attack rate</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Pitching_Moment_Due_To_Elevator</td>
<td>Pitching moment due to elevator</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Yawing_Moment_Due_To_Rudder</td>
<td>yawing moment due to rudder</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Oscillatory_Roll_Rate</td>
<td>Oscillatory roll rate</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Oscillatory_Pitch_Rate</td>
<td>Oscillatory pitch rate</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Oscillatory_Yaw_Rate</td>
<td>Oscillatory yaw rate</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Oscillatory_Roll_Rate_Stability_Derivative</td>
<td>Oscillatory roll rate stab. deriv.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Oscillatory_Yaw_Rate_Stability_Derivative</td>
<td>Oscillatory yaw rate stab. deriv.</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Last_Times_Linear_Velocity</td>
<td>linear velocities from N-1 (array)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Last_Times_Angular_Position</td>
<td>previous angular position VECTOR</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Last_Times_Angular_Velocity</td>
<td>angular velocity VECTOR (N-1)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Last_Times_Angular_Acceleration</td>
<td>angular accelration VECTOR (N-1)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Fuel_X_Moment</td>
<td>array of x-momt for each tank (array)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Fuel_Y_Moment</td>
<td>array of y-momt for each tank (array)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Fuel_Z_Moment</td>
<td>array of z-momt for each tank (array)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Total_X_Moments</td>
<td>total x moments</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Total_Y_Moments</td>
<td>total y moments</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Total_Z_Moments</td>
<td>total z moments</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Cargo_X_Position</td>
<td>cargo x position</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Cargo_Y_Position</td>
<td>cargo y position</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Cargo_Z_Position</td>
<td>cargo z position</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Cargo_X_Moment</td>
<td>cargo x moment</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Cargo_Y_Moment</td>
<td>cargo y moment</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Cargo_Z_Moment</td>
<td>cargo z moment</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Aircraft_Empty_Weight_X_Moment</td>
<td>A/C empty weight x moment</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Aircraft_Empty_Weight_Y_Moment</td>
<td>A/C empty weight y moment</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Aircraft_Empty_Weight_Z_Moment</td>
<td>A/C empty weight z moment</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Total_Ground_Reaction_Body_Axis_X_Force</td>
<td>Total ground reaction x force (body axis)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Total_Ground_Reaction_Body_Axis_Y_Force</td>
<td>Total ground reaction y force (body axis)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Total_Ground_Reaction_Body_Axis_Z_Force</td>
<td>Total ground reaction z force (body axis)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Total_Ground_Reaction_Body_Axis_Rolling_Moment</td>
<td>Total ground reaction pitch momt (body axis)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Total_Ground_Reaction_Body_Axis_Pitching_Moment</td>
<td>Total ground reaction roll momt (body axis)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Total_Ground_Reaction_Body_Axis_Yawing_Moment</td>
<td>Total ground reaction yaw momt (body axis)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td>Engine_Thrust</td>
<td>array of engine thrusts (array)</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td>Thrust_Coefficient</td>
<td>Thrust coefficient</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
</tbody>
</table>

KEY TO LISTING ABBREVIATIONS

Notes: (1) Axis Systems Used:

GE = Geo-centric earth fixed axis sytem which is the

ANSI/AIAA 1.1.3 Geocentric Earth-fixed axis system \[Ref 10\]

DIS Geocentric Cartesian Coordinate System (also referred to as World
Coordinate System) \[Ref. 38\]

The DIS and AIAA axis systems are identical.

Rotating Earth with axis system origin at Earth\'s center, X(GE) axis
intersects the surface at Greenwich Meridian and the Equator,

Z (GE) axis is cooincindent with the Earth\'s spin axis North, and Y
(GE)axis completing the right handed triad.

When referred to in a variable name it is \...\_GE\_\... and in a symbol
it is (GE). The parenthesis indicating

the letters GE refer to an axis system.

\(2\) NASA Ames\[Ref 39\] , DIS \[Ref 38\], ANSI/AIAA \[ref 10\], and
NAWC-TSD agree on this definition,

This is a generally accepted definition.

\(3\) NASA Ames\[Ref 39\] , ANSI/AIAA \[ref 10\], and NAWC-TSD agree on
this definition. Not defined by DIS.

This is a generally accepted definition.

\(4\) Axis Systems Used:

FE (flat earth or local) frame is defined by NASA Ames \[Ref. 10\] as:

The Local (L) frame is situatied on the earth\'s surface, directly under
the vehicle. Its XL axis points Northward

and its Y(L) axis points Eastward: both are paralel to the Earths\'s
surface.

The Z(L) axis pointstowards the Earth\'s center. It moves with the
aircraft, the -Z(L) axis passes through the aircraft cg.

Since it move with the aircraft it is not an inertiaFE (flat earth or
local) frame. The LocaFE (flat earth or local) frame\'s origin is always
a constant

distance from the Earth\'s center.

\(5\) Axis Systems Used:

B = Body Axis

which both ANSI/AIAA \[Ref 10, 1.1.7\] and NASA Ames \[Ref 39\] call
\"Body Axis\" and DIS calls \"Entity Coordinate System\'

\[Ref 38\]. All definitions are identical and normally accepted
throughout industry.

The origin of the Body axis system is at the CG of the vehicle.

The X(B) axis passes is parallel to the horizontal (XY) reference plane
of the vehicle and is positive forward,

The Y(B) axis is parallel to the horizontal (XY) reference plane and is
positive to the right.

The Z(B) axis is positive down, completing the right handed triad.

When referred to in a variable name it is \...\_B\_\... and in a symbol
it is (B). The parenthesis indicating

the letter B refers to an axis system.

  ----- ------- ---- --------- ------------------------- ---------------- ------- ---- ---- ---- ----- -- ----
  84    FLOAT        XPR                                 Distance Of      DOWN                            
        32 BITS                                          Pilot Down                                       
                                                         Runway                                           

  85    FLOAT        YPR                                 Distance Of      RIGHT                           
        32 BITS                                          Pilot To Right                                   
                                                         Of Rwy                                           

  86    FLOAT        HPR                                 Height Of Pilot  UP                              
        32 BITS                                          Above Runway                                     

  87    FLOAT        DNR                                 Aircraft         NORTH                           
        32 BITS                                          Distance North                                   
                                                         Of Runway                                        

  88    FLOAT        DER                                 Aircraft         EAST                            
        32 BITS                                          Distance East Of                                 
                                                         Runway                                           

  89    FLOAT        HDG_RWY   Active_Runway_Heading_d   Compass heading                                  
        32 BITS                                          of current                                       
                                                         runway                                           

  90    FLOAT        XRUNWAY                             X-position in    NORTH                           
        32 BITS                                          NED of runway                                    
                                                         (latitude)                                       

  91    FLOAT        YRUNWAY                             Y-location in    EAST                            
        32 BITS                                          NED of runway                                    
                                                         (longitude)                                      

  92    FLOAT        CLATR                               Cosine Of Runway NORTH                           
        32 BITS                                          Latitude                                         

  93    FLOAT        SHDGRWY                             Sine of runway                                   
        32 BITS                                          compass heading                                  

  94    FLOAT        CHDGRWY                             Cosine of runway                                 
        32 BITS                                          compass heading                                  

  119   FLOAT        FN                                  Total Force,     NORTH                           
        32 BITS                                          North Axis                                       

  120   FLOAT        FE                                  Total Force,     EAST                            
        32 BITS                                          East Axis                                        

  121   FLOAT        FD                                  Total Force,     DOWN                            
        32 BITS                                          Down Axis                                        

  122   FLOAT   FG   FG        Gravitational_Force_lbf   Total Force Due  n                               
        32 BITS                                          To Gravity (at                                   
                                                         Alt.)                                            
  ----- ------- ---- --------- ------------------------- ---------------- ------- ---- ---- ---- ----- -- ----