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Aerodynamics and Flight Dynamics
Mission Analysis
MSA Toolkit
Commits
5f813f0b
Commit
5f813f0b
authored
2 months ago
by
Marco Luigi Gaibotti
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[updates] Removed longitudinal and lateral xcps from prints
parent
fcbcce86
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1 merge request
!21
[updates] Removed longitudinal and lateral xcps from prints
Pipeline
#11448
failed
2 months ago
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2
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3
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common
+1
-1
1 addition, 1 deletion
common
simulator/src/prints.m
+2
-4
2 additions, 4 deletions
simulator/src/prints.m
with
3 additions
and
5 deletions
common
@
59b6c1b0
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7eab4272
...
59b6c1b0
Subproject commit
7eab42722e6f7e0576f77383b27bfcd614096e88
Subproject commit
59b6c1b09cbd9b1bc1be07e1aa32f18ced11e1bc
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simulator/src/prints.m
+
2
−
4
View file @
5f813f0b
...
@@ -66,9 +66,7 @@ maxTemperature = (externalTemp*(1+(((gamma-1)/2)*(mach(iMaxV)^2))))-273.15;
...
@@ -66,9 +66,7 @@ maxTemperature = (externalTemp*(1+(((gamma-1)/2)*(mach(iMaxV)^2))))-273.15;
% XCPor = ascent.coeff.XCPor(~isnan(ascent.coeff.XCPor)); % keeping the NaN elements in ascent.coeff.XCPor, but not in XCPor
% XCPor = ascent.coeff.XCPor(~isnan(ascent.coeff.XCPor)); % keeping the NaN elements in ascent.coeff.XCPor, but not in XCPor
% end
% end
% longitudinal XCPs
% XCP
lonXCPs
=
-
ascent
.
coeff
.
XCPlon
(
~
isnan
(
ascent
.
coeff
.
XCPlon
));
latXCPs
=
-
ascent
.
coeff
.
XCPlat
(
~
isnan
(
ascent
.
coeff
.
XCPlat
));
totXCPs
=
ascent
.
coeff
.
XCPtot
(
~
isnan
(
ascent
.
coeff
.
XCPtot
));
totXCPs
=
ascent
.
coeff
.
XCPtot
(
~
isnan
(
ascent
.
coeff
.
XCPtot
));
% DATA RECORD (display)
% DATA RECORD (display)
...
@@ -101,7 +99,7 @@ fprintf('speed at launch pad exit: %g [m/s] \n', absV(iExit))
...
@@ -101,7 +99,7 @@ fprintf('speed at launch pad exit: %g [m/s] \n', absV(iExit))
% else
% else
% fprintf('Stability margin at launchpad exit [-]:\n Lon: %g\n Lat: %g\n Tot: %g\n', lonXCPs(1), latXCPs(1), totXCPs(1))
% fprintf('Stability margin at launchpad exit [-]:\n Lon: %g\n Lat: %g\n Tot: %g\n', lonXCPs(1), latXCPs(1), totXCPs(1))
% end
% end
fprintf
(
'Stability margin at launchpad exit [-]:\n Lon: %g\n Lat: %g\n Tot: %g\n'
,
lonXCPs
(
1
),
latXCPs
(
1
),
totXCPs
(
1
))
fprintf
(
'Stability margin at launchpad exit [-]:\n Lon: %g\n Lat: %g\n Tot: %g\n'
,
totXCPs
(
1
))
fprintf
(
'time: %g [sec] \n\n'
,
time
(
iExit
))
fprintf
(
'time: %g [sec] \n\n'
,
time
(
iExit
))
fprintf
(
'latitude of landing point: %10.8f [deg] \n'
,
lat
(
end
));
fprintf
(
'latitude of landing point: %10.8f [deg] \n'
,
lat
(
end
));
...
...
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