Datasets:
SM-Bello
/
C172P-Grounded-JSBSim-Airborne-Trim-Failure-Negative-Result

Dataset card Data Studio Files
xet
 Community
1
text
stringclasses
539 values
Function: aero/coefficient/CLq
1 dimensional table with 3 rows.
-0.349 0.0322
0 0
0.349 -0.0322
Function: aero/coefficient/Clb
Function: aero/coefficient/Clp
2 dimensional table with 2 rows, 2 columns.
0 30
0 0.0798 0.1246
0.094 0.1869 0.2317
Function: aero/coefficient/Clr
Function: aero/coefficient/ClDa
Function: aero/coefficient/Cldr
Function: aero/coefficient/Cmo
Function: aero/coefficient/Cmalpha
Function: aero/coefficient/Cmq
Function: aero/coefficient/Cmadot
Function: aero/coefficient/Cmde
1 dimensional table with 4 rows.
0 0
10 -0.0654
20 -0.0981
30 -0.114
Function: aero/coefficient/Cmdf
1 dimensional table with 3 rows.
-0.349 -0.0205
0 0
0.349 0.0205
Function: aero/coefficient/Cnb
Function: aero/coefficient/Cnp
Function: aero/coefficient/Cnr
Function: aero/coefficient/Cnda
Function: aero/coefficient/Cndr
Mass Properties Report (English units: lbf, in, slug-ft^2)
Weight CG-X CG-Y CG-Z Ixx Iyy Izz Ixy Ixz Iyz
Base Vehicle 1500.0 41.0 0.0 36.5 948.0 1346.0 1967.0 0.0 -0.0 0.0
0 Pilot 180.0 36.0 -14.0 24.0 0.0 0.0 0.0 -0.0 0.0 -0.0
1 Co-Pilot 0.0 36.0 14.0 24.0 0.0 0.0 0.0 -0.0 0.0 -0.0
2 Left Passenger 0.0 70.0 -14.0 24.0 0.0 0.0 0.0 -0.0 0.0 -0.0
3 Right Passenger 0.0 70.0 14.0 24.0 0.0 0.0 0.0 -0.0 0.0 -0.0
4 Baggage 0.0 95.0 0.0 24.0 0.0 0.0 0.0 -0.0 0.0 -0.0
0 Fuel  100 56 -112 59.4 0 0 0
1 Fuel  100 56 112 59.4 0 0 0
Total: 1880.0 42.1 -1.3 37.7 1524.5 1384.3 2525.6 3.3 -16.7 7.5
End of vehicle configuration loading.
-------------------------------------------------------------------------------
t= 0.0s h= 1000.0ft theta=+2.00deg elev=+0.004 thr=0.003
t= 5.0s h= 998.5ft theta=+0.48deg elev=+0.132 thr=0.650
t= 10.0s h= 986.7ft theta=+0.50deg elev=+0.123 thr=0.650
t= 15.0s h= 971.4ft theta=+0.40deg elev=+0.104 thr=0.650
t= 20.0s h= 949.5ft theta=+0.20deg elev=+0.074 thr=0.650
t= 25.0s h= 918.1ft theta=-0.16deg elev=+0.024 thr=0.650
[RESULT] gear_contact occurred: False
[RESULT] final altitude: 872.1ft (delta=-127.9ft)
[DONE]
PHI-CTRL c172p negative-result dataset -- environment capture
=================================================================
jsbsim python package version : 1.3.1
jsbsim FDM reported version : 1.3.1 May 17 2026 14:26:04
python version : 3.12.3 (main, Mar 3 2026, 12:15:18) [GCC 13.3.0]
platform : Linux-6.18.44-fc-v22-x86_64-with-glibc2.39
processor : x86_64
c172p.xml path : /usr/local/lib/python3.12/dist-packages/jsbsim/aircraft/c172p/c172p.xml
c172p.xml sha256 : 0af58c613f7bca7e1d85f4b2e178a4d7b0b14dda6d5f79b38c571d9911187aa4
NOTE: c172p.xml is bundled with the pip jsbsim package at the
version above (installed via `pip install jsbsim`, unmodified).
No separate jsbsim-aircraft GitHub commit hash is available for
this file since it was not cloned from that repo independently --
the sha256 above is the authoritative identifier for exactly which
aircraft definition produced the results in this dataset.