Initial commit.

.gitignore

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+build
+*.swp
+.nfs*
+*.blend1
+initfile.xml

CMakeLists.txt

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+project (arkhangar)
+
+# Requried cmake version
+cmake_minimum_required (VERSION 2.8.2)
+set(PROJECT_VERSION_MAJOR "1")
+set(PROJECT_VERSION_MINOR "3")
+set(PROJECT_VERSION_PATCH "0")
+set(PROJECT_VERSION "${PROJECT_VERSION_MAJOR}.${PROJECT_VERSION_MINOR}.${PROJECT_VERSION_PATCH}")
+set(PROJECT_CONTACT_EMAIL [email protected])
+set(PROJECT_CONTACT_VENDOR arkTools)
+set(LIBRARY_VERSION ${PROJECT_VERSION})
+set(LIBRARY_SOVERSION "0.0.0")
+
+# config files
+configure_file(config.h.in config.h)
+install(FILES ${CMAKE_BINARY_DIR}/config.h DESTINATION share/${PROJECT_NAME} COMPONENT Runtime)
+
+# install files
+install(DIRECTORY aircraft/ DESTINATION share/${PROJECT_NAME}/aircraft)
+install(DIRECTORY analysis/ DESTINATION share/${PROJECT_NAME}/analysis)
+install(DIRECTORY scripts/ DESTINATION share/${PROJECT_NAME}/scripts)
+
+### packaging
+
+# add file extensions and set resource files
+configure_file("COPYING" "COPYING.txt" COPYONLY)
+configure_file("README" "README.txt" COPYONLY)
+set(CPACK_RESOURCE_FILE_LICENSE "${CMAKE_BINARY_DIR}/COPYING.txt")
+set(CPACK_RESOURCE_FILE_README "${CMAKE_BINARY_DIR}/README.txt")
+set(CPACK_PACKAGE_DESCRIPTION_FILE "${CPACK_RESOURCE_FILE_README}")
+set(CPACK_RESOURCE_FILE_WELCOME "${CMAKE_SOURCE_DIR}/cmake/WELCOME.txt")
+set(CPACK_PACKAGE_DESCRIPTION_SUMMARY "arktools aircraft hangar")
+set(CPACK_PACKAGE_VENDOR ${PROJECT_CONTACT_VENDOR})
+set(CPACK_PACKAGE_CONTACT "${PROJECT_CONTACT_EMAIL}")
+set(CPACK_PACKAGE_VERSION ${PROJECT_VERSION})
+set(CPACK_SET_DESTDIR TRUE)
+set(CPACK_COMPONENTS_GROUPING "ALL_COMPONENTS_IN_ONE")
+set(CPACK_DEBIAN_PACKAGE_DEPENDS "")
+set(CPACK_PACKAGE_EXECUTABLES "")
+include(CPack)
+
+# vim:sw=4:ts=4:expandtab

README

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+This is the arktools aircraft hanger. It can be used by JSBSim or FlightGear for simulating and visualizing aircraft.

aircraft/arducopter/Engines/a2830-12.xml

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+<?xml version="1.0"?>
+<electric_engine name="a2830-12">
+  <power unit="WATTS">  187 </power>
+</electric_engine>

aircraft/arducopter/Engines/prop10x4.5.xml

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+<?xml version="1.0"?>
+<!-- Generated by Aero-Matic v 1.1
+
+     Inputs:
+                horsepower: 0.250767
+                     pitch: fixed
+            max engine rpm: 9435
+        prop diameter (ft): 0.83333333333333
+
+     Outputs:
+              max prop rpm: 22515.60
+                gear ratio:    0.42
+                       Cp0: 0.002731
+                       Ct0: 0.003823
+       static thrust (lbs):    0.66
+-->
+<propeller name="prop">
+  <!--<ixx>   0.00 </ixx>-->
+  <ixx>   0.000041666666 </ixx>
+  <!--assuming solid rod of mass 8 g-->
+  <diameter unit="IN">  10.0 </diameter>
+  <numblades> 2 </numblades>
+  <gearratio>  1.0 </gearratio>
+  <p_factor>   0.79 </p_factor>
+  <table name="C_THRUST" type="internal">
+    <tableData><!--experimentally measured-->
+			0.0 0.0054513
+			1.4 0.0054513
+			<!--aeromatic generated-->
+            <!--0.0   0.0042-->
+            <!--0.1   0.0040-->
+            <!--0.2   0.0038-->
+            <!--0.3   0.0035-->
+            <!--0.4   0.0032-->
+            <!--0.5   0.0028-->
+            <!--0.6   0.0023-->
+            <!--0.7   0.0017-->
+            <!--0.8   0.0009-->
+            <!--1.0  -0.0003-->
+            <!--1.2  -0.0016-->
+            <!--1.4  -0.0030-->
+        </tableData>
+  </table>
+  <table name="C_POWER" type="internal">
+    <tableData>
+            0.0   0.0028
+            0.1   0.0028
+            0.2   0.0027
+            0.3   0.0027
+            0.4   0.0025
+            0.5   0.0023
+            0.6   0.0021
+            0.7   0.0018
+            0.8   0.0015
+            1.0   0.0005
+            1.2  -0.0008
+            1.4  -0.0025
+            1.6  -0.0042
+        </tableData>
+  </table>
+  <!-- thrust effects of helical tip Mach -->
+  <table name="CT_MACH" type="internal">
+    <tableData>
+            0.85   1.0
+            1.05   0.8
+        </tableData>
+  </table>
+  <!-- power-required effects of helical tip Mach -->
+  <table name="CP_MACH" type="internal">
+    <tableData>
+            0.85   1.0
+            1.05   1.8
+            2.00   1.4
+        </tableData>
+  </table>
+</propeller>