diff --git a/files/pixhawk/hexarotor/widgets/mavconn.qgw b/files/pixhawk/hexarotor/widgets/mavconn.qgw
deleted file mode 100644
index ff33f3786baccbb9cf2237611ab28dc946c90b8a..0000000000000000000000000000000000000000
--- a/files/pixhawk/hexarotor/widgets/mavconn.qgw
+++ /dev/null
@@ -1,62 +0,0 @@
-[MAVCONN%20Control]
-QGC_TOOL_WIDGET_ITEMS\1\TYPE=COMMANDBUTTON
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_DESCRIPTION=DO: Control Video
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_BUTTONTEXT=CAPTURE
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_COMMANDID=200
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAMS_VISIBLE=false
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM1=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM2=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM3=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM4=2
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM5=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM6=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM7=0
-QGC_TOOL_WIDGET_ITEMS\2\TYPE=COMMANDBUTTON
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_DESCRIPTION=DO: Control Video
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_BUTTONTEXT=STOP
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_COMMANDID=200
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAMS_VISIBLE=false
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM1=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM2=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM3=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM4=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM5=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM6=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM7=0
-QGC_TOOL_WIDGET_ITEMS\3\TYPE=COMMANDBUTTON
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_DESCRIPTION=PREFLIGHT: Calibration
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_BUTTONTEXT=CALIBRATE
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_COMMANDID=241
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAMS_VISIBLE=false
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM1=1
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM2=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM3=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM4=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM5=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM6=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM7=0
-QGC_TOOL_WIDGET_ITEMS\4\TYPE=SLIDER
-QGC_TOOL_WIDGET_ITEMS\4\QGC_PARAM_SLIDER_DESCRIPTION=Setpoint ON<->OFF
-QGC_TOOL_WIDGET_ITEMS\4\QGC_PARAM_SLIDER_PARAMID=
-QGC_TOOL_WIDGET_ITEMS\4\QGC_PARAM_SLIDER_COMPONENTID=0
-QGC_TOOL_WIDGET_ITEMS\4\QGC_PARAM_SLIDER_MIN=1
-QGC_TOOL_WIDGET_ITEMS\4\QGC_PARAM_SLIDER_MAX=0
-QGC_TOOL_WIDGET_ITEMS\5\TYPE=SLIDER
-QGC_TOOL_WIDGET_ITEMS\5\QGC_PARAM_SLIDER_DESCRIPTION=Glob. Loc ON<->OFF
-QGC_TOOL_WIDGET_ITEMS\5\QGC_PARAM_SLIDER_PARAMID=
-QGC_TOOL_WIDGET_ITEMS\5\QGC_PARAM_SLIDER_COMPONENTID=0
-QGC_TOOL_WIDGET_ITEMS\5\QGC_PARAM_SLIDER_MIN=1
-QGC_TOOL_WIDGET_ITEMS\5\QGC_PARAM_SLIDER_MAX=0
-QGC_TOOL_WIDGET_ITEMS\6\TYPE=SLIDER
-QGC_TOOL_WIDGET_ITEMS\6\QGC_PARAM_SLIDER_DESCRIPTION=GPS ENU HL<->ASL
-QGC_TOOL_WIDGET_ITEMS\6\QGC_PARAM_SLIDER_PARAMID=
-QGC_TOOL_WIDGET_ITEMS\6\QGC_PARAM_SLIDER_COMPONENTID=0
-QGC_TOOL_WIDGET_ITEMS\6\QGC_PARAM_SLIDER_MIN=0
-QGC_TOOL_WIDGET_ITEMS\6\QGC_PARAM_SLIDER_MAX=1
-QGC_TOOL_WIDGET_ITEMS\7\TYPE=SLIDER
-QGC_TOOL_WIDGET_ITEMS\7\QGC_PARAM_SLIDER_DESCRIPTION=Yaw PX<->ASL
-QGC_TOOL_WIDGET_ITEMS\7\QGC_PARAM_SLIDER_PARAMID=
-QGC_TOOL_WIDGET_ITEMS\7\QGC_PARAM_SLIDER_COMPONENTID=0
-QGC_TOOL_WIDGET_ITEMS\7\QGC_PARAM_SLIDER_MIN=0
-QGC_TOOL_WIDGET_ITEMS\7\QGC_PARAM_SLIDER_MAX=1
-QGC_TOOL_WIDGET_ITEMS\size=7
diff --git a/files/pixhawk/quadrotor/parameter_tooltips/tooltips.txt b/files/pixhawk/quadrotor/parameter_tooltips/tooltips.txt
deleted file mode 100644
index 610873647651e034a665f5d2d85dd53cf41a8a47..0000000000000000000000000000000000000000
--- a/files/pixhawk/quadrotor/parameter_tooltips/tooltips.txt
+++ /dev/null
@@ -1,3 +0,0 @@
-EEPROM,variable name,Min,Max,Default,Multiplier,Enabled (0 = no, 1 = yes),Comment
-HDNG2RLL_P, 0, 5, 0.7, 1, 1, NAV_ROLL_P - Navigation control gains. Tuning values for the navigation control PID loops. The P term is the primary tuning value. This determines how the control deflection varies in proportion to the required correction.
-SYS_TYPE, 0, 15, 1, 1, 1, System type (airframe)
\ No newline at end of file
diff --git a/files/pixhawk/quadrotor/widgets/mavconn.qgw b/files/pixhawk/quadrotor/widgets/mavconn.qgw
deleted file mode 100644
index e7b6e644f1ec9a866d50d7bec4aedd9fcf7e4d94..0000000000000000000000000000000000000000
--- a/files/pixhawk/quadrotor/widgets/mavconn.qgw
+++ /dev/null
@@ -1,38 +0,0 @@
-[MAVCONN%20Control]
-QGC_TOOL_WIDGET_ITEMS\1\TYPE=COMMANDBUTTON
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_DESCRIPTION=START Recording
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_BUTTONTEXT=CAPTURE
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_COMMANDID=200
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAMS_VISIBLE=false
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM1=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM2=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM3=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM4=2
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM5=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM6=0
-QGC_TOOL_WIDGET_ITEMS\1\QGC_COMMAND_BUTTON_PARAM7=0
-QGC_TOOL_WIDGET_ITEMS\2\TYPE=COMMANDBUTTON
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_DESCRIPTION=STOP Recording
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_BUTTONTEXT=STOP
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_COMMANDID=200
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAMS_VISIBLE=false
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM1=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM2=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM3=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM4=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM5=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM6=0
-QGC_TOOL_WIDGET_ITEMS\2\QGC_COMMAND_BUTTON_PARAM7=0
-QGC_TOOL_WIDGET_ITEMS\3\TYPE=COMMANDBUTTON
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_DESCRIPTION=PREFLIGHT: Calibration
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_BUTTONTEXT=CALIBRATE
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_COMMANDID=241
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAMS_VISIBLE=false
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM1=1
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM2=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM3=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM4=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM5=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM6=0
-QGC_TOOL_WIDGET_ITEMS\3\QGC_COMMAND_BUTTON_PARAM7=0
-QGC_TOOL_WIDGET_ITEMS\size=3
diff --git a/files/px4/parameter_tooltips/tooltips.txt b/files/px4/parameter_tooltips/tooltips.txt
deleted file mode 100644
index 854f5a0162b25c750085b561f4a88b33ab53282c..0000000000000000000000000000000000000000
--- a/files/px4/parameter_tooltips/tooltips.txt
+++ /dev/null
@@ -1,11 +0,0 @@
-^ Name            ^ Min    ^ Max    ^ Default  ^ Multiplier  ^ Enabled ^  Comment ^
-| BAT_V_EMPTY     | 0.9    | 100.0  | 3.2      | 1           | 1       | Voltage of an empty battery cell  |
-| BAT_V_FULL      | 1.0    | 200.0  | 4.05     | 1           | 1       | Voltage of a full battery cell    |
-| BAT_N_CELLS     | 1      | 100    | 3        | 1           | 1       | Number of SERIAL battery cells. Typically this ranges from 2S to 6S in small-scale UAVs  |
-| BAT_V_SCALING   | 0.001  | 1.0    | 0.00838  | 1           | 1       | Conversion from ADC ticks to battery voltage. Depends on the connected board, calibrate with a multimeter.  |
-| MC_ATTRATE_P    | 0.0    | 20.0   | 0.20     | 1           | 1       | Multirotor attitude rate control P gain. This gain controls how much of the motor thrust should be used to control angular velocity. A larger number will increase the control response, but will make the system also more twitchy. |
-| MC_ATTRATE_D    | 0.0    | 20.0   | 0.05     | 1           | 1       | Multirotor attitude rate control D gain. A large value will allow to damp oscillations due to a high P gain, but will make the system response suspectible to noise.|
-| MC_ATT_P    | 0.0    | 20.0   | 0.20     | 1           | 1       | Multirotor attitude control proportional (P) gain. This defines how strong the response of the system will be to an attitude error|
-| MC_ATT_D    | 0.0    | 20.0   | 0.05     | 1           | 1       | Multirotor attitude control D gain. A large value will allow to damp oscillations due to a high P gain, but will make the system response suspectible to noise.|
-| FW_ROLLRATE_P    | 0.0    | 20.0   | 0.30     | 1           | 1       | Fixed wing roll rate control P gain. This gain controls how strong the ailerons or rudder should be actuated in order to achieve a certain roll rate. A larger number will increase the control response, but will make the system also more twitchy. |
-| FW_HEADING_P    | 0.0    | 20.0   | 4.00     | 1           | 1       | Fixed wing heading error to bank angle gain |
\ No newline at end of file