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ebouhoubeiny / cpacs

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Add Flight Dynamics #390

Open GoogleCodeExporter opened 8 years ago

GoogleCodeExporter commented 8 years ago 
Add flight dynamics elements as a further branch to the analysis node. Get in 
contact with Gertjan and Jana for documentation. 

          <flightDynamics>
            <flightCases>
              <flightCase uID="D150_VAMP_takeoff_fCG">
                <name>takeoff_fCG</name>
                <description>takeoff with MTOW and forward CG position</description>
                <weightAndBalanceUID>101pay_050fuel</weightAndBalanceUID>
                <standardAltitude>300.0</standardAltitude>
                <vCAS>90.0</vCAS>
                <configuration>0</configuration>
                <gear>0</gear>
              </flightCase>
              <flightCase uID="D150_VAMP_takeoff_mCG">
                <name>takeoff_mCG</name>
                <description>takeoff with MTOW and intermediate CG position</description>
                <weightAndBalanceUID>050pay_100fuel</weightAndBalanceUID>
                <standardAltitude>300.0</standardAltitude>
                <vCAS>90.0</vCAS>
                <configuration>0</configuration>
                <gear>0</gear>
              </flightCase>
              <flightCase uID="D150_VAMP_takeoff_aCG">
                <name>takeoff_aCG</name>
                <description>takeoff with MTOW and aft CG position</description>
                <weightAndBalanceUID>102pay_050fuel</weightAndBalanceUID>
                <standardAltitude>300.0</standardAltitude>
                <vCAS>90.0</vCAS>
                <configuration>0</configuration>
                <gear>0</gear>
              </flightCase>
              <flightCase uID="D150_VAMP_cruise_fCG">
                <name>cruise_fCG</name>
                <description>cruise with MTOW and forward CG position</description>
                <weightAndBalanceUID>101pay_050fuel</weightAndBalanceUID>
                <standardAltitude>10500.0</standardAltitude>
                <vCAS>138.0</vCAS>
                <configuration>0</configuration>
                <gear>0</gear>
                <linearModel>
                  <Alon>0 1.832499495421754e-006 -0.001135914961633912 0 -2.709370215739938e-006 -0.04893627279951512 -0.002150872945703369 -0.08522401349307811 0 0.001075055002393592 0.9988019028706372 0.05221051699505656 -0.5256634720527089 0 -0.02309095181792761 -232.2562404554244 -9.78152457269777 -0.4789480226980721 0 7.076543402657636e-007 0 -11.53353053783087 227.4077271380522 1 -1.206766805517581</Alon>
                  <Blon>0 -0.05558478087274257 -3.281284232093818 0 -1.261495006993593 0 -2.424885431443529e-005 -0.001431460182616635 0 -0.0005503271977005558</Blon>
                  <Clon>0 -1.000001540650492 0 1.235726496974087e-010 0 0 0.0001159894933723115 0 0 0 0.9988018345402289 -0.0002106994964462684 0.000210699483839158 0.00870231527999827 0 0 0 0.04893625743476307 0.004300430857777908 -0.004300430600499165 0.05367606041512612 0 -4.656384915909346e-005 1.000000000014397 1.42101590451335e-009 6.938554221256593e-013 0.9999999402590893 -3.037697372813123e-005 1 0 0 0 0 0 0.4666728991797874</Clon>
                  <Dlon>0 0 0 0 0 0 0.3350554490821573 0 0 0 0 0 0 0.0001461679388636838</Dlon>
                  <Alat>-0.03569935936298644 0 0 -0.02752565437665752 0.01017227761998301 9.781524054830996 0 0 9.991365561081638e-012 -3.246252281427003e-012 -7.741826833146725e-012 0 0 1.012735211118975e-012 1.557752770151976e-012 11.06745772052288 1 0 -2.172952420465644 0.08956690020902829 -230.8910959124612 0.04899497353445802 1.001199534274583 0.595524525471439 -0.3170432597582324</Alat>
                  <Blat>0.1407926446338744 0 0 1.778387410134996 -0.07203045150838969 -2.806581038411989 0 0 -0.8316068036912072 0.848296430247342 6.14207910720919e-005 0 0 0.0007758215072182623 -3.142328439632133e-005 -0.01224581471618429 0 0 -0.003628508386284203 0.003701329399351502</Blat>
                  <Clat>0 0 0 0 0.004305588851982897 0.004305588851451681 0.003645299839070712 0 0 0.9999999999982814 2.220446049250313e-011 -2.106062720053092e-012 -0.04893627274515921 -3.037371909362077e-012 0 0 5.548550227229801e-012 1.00000000000548 9.525144965191375e-013 1.000000000016564 6.170554329485489e-012 1 0 0 0 0 0 0.03045942766387301 0 1 0 0 0 0 -0.1109823809349067</Clat>
                  <Dlat>0 0 0 0 0 0 -0.01437648781334511 0 0 0 0 0 0 0.2865829972923714 0 0 0 0 0 0 -6.271742793312762e-006 0 0 0 0 0 0 0.00125043326296996</Dlat>
                </linearModel>
                <trimResult>
                  <mach>0.781285633712503</mach>
                  <vTAS>232.256254337782</vTAS>
                  <alpha>2.804962189544282</alpha>
                  <altitude>10500.00000115018</altitude>
                </trimResult>
              </flightCase>
              <flightCase uID="D150_VAMP_cruise_aCG">
                <name>cruise_aCG</name>
                <description>cruise with MTOW and aft CG position</description>
                <weightAndBalanceUID>102pay_050fuel</weightAndBalanceUID>
                <standardAltitude>10500.0</standardAltitude>
                <vCAS>138.0</vCAS>
                <configuration>0</configuration>
                <gear>0</gear>
              </flightCase>
              <flightCase uID="D150_VAMP_approach_fCG">
                <name>approach_fCG</name>
                <description>approach with MLW and forward CG position</description>
                <weightAndBalanceUID>101pay_010fuel</weightAndBalanceUID>
                <standardAltitude>600.0</standardAltitude>
                <vCAS>80.0</vCAS>
                <configuration>3</configuration>
                <gear>1</gear>
              </flightCase>
              <flightCase uID="D150_VAMP_approach_aCG">
                <name>approach_aCG</name>
                <description>approach with MLW and aft CG position</description>
                <weightAndBalanceUID>102pay_010fuel</weightAndBalanceUID>
                <standardAltitude>600.0</standardAltitude>
                <vCAS>80.0</vCAS>
                <configuration>3</configuration>
                <gear>1</gear>
              </flightCase>
              <flightCase uID="D150_VAMP_FlightCaseNominal">
                <name>name</name>
                <description>description</description>
                <weightAndBalanceUID>102pay_050fuel</weightAndBalanceUID>
                <standardAltitude>5000.0</standardAltitude>
                <vCAS>150.0</vCAS>
                <configuration>0</configuration>
                <gear>0</gear>
              </flightCase>
            </flightCases>
            <modelDescription>
              <description>Model from FDS prepared for HAREM.</description>
              <xLonNames>z_E [m];u_B [m/s];w_B [m/s];Theta [rad];qb [rad/s]</xLonNames>
              <yLonNames>qb [rad/s];h (WGS) [m];Theta [rad];Vtas [m/s];alpha [rad];gamma [rad];nz [-]</yLonNames>
              <uLonNames>dqCommand [rad];stickPitch [N]</uLonNames>
              <xLatNames>v_B [m/s];Phi [rad];Psi [rad];pb [rad/s];rb [rad/s]</xLatNames>
              <yLatNames>pb [rad/s];rb [rad/s];Phi [rad];Psi [rad];beta [rad];chi [rad];ny [-]</yLatNames>
              <uLatNames>dpCommand [rad];drCommand [rad];stickRoll [N];pedals [N]</uLatNames>
            </modelDescription>
          </flightDynamics>

Original issue reported on code.google.com by daniel.b...@googlemail.com on 9 Jul 2014 at 8:30

GoogleCodeExporter commented 8 years ago

Original comment by daniel.b...@googlemail.com on 28 Jan 2015 at 12:24