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// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Copyright (c) Holger Buss, Ingo Busker
// + Nur für den privaten Gebrauch
// + www.MikroKopter.com
// + porting the sources to other systems or using the software on other systems (except hardware from www.mikrokopter.de) is not allowed
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Es gilt für das gesamte Projekt (Hardware, Software, Binärfiles, Sourcecode und Dokumentation),
// + dass eine Nutzung (auch auszugsweise) nur für den privaten (nicht-kommerziellen) Gebrauch zulässig ist.
// + Sollten direkte oder indirekte kommerzielle Absichten verfolgt werden, ist mit uns (info@mikrokopter.de) Kontakt
// + bzgl. der Nutzungsbedingungen aufzunehmen.
// + Eine kommerzielle Nutzung ist z.B.Verkauf von MikroKoptern, Bestückung und Verkauf von Platinen oder Bausätzen,
// + Verkauf von Luftbildaufnahmen, usw.
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder veröffentlicht,
// + unterliegen sie auch diesen Nutzungsbedingungen und diese Nutzungsbedingungen incl. Copyright müssen dann beiliegen
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts
// + auf anderen Webseiten oder sonstigen Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de"
// + eindeutig als Ursprung verlinkt werden
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Keine Gewähr auf Fehlerfreiheit, Vollständigkeit oder Funktion
// + Benutzung auf eigene Gefahr
// + Wir übernehmen keinerlei Haftung für direkte oder indirekte Personen- oder Sachschäden
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Die Portierung der Software (oder Teile davon) auf andere Systeme (ausser der Hardware von www.mikrokopter.de) ist nur
// + mit unserer Zustimmung zulässig
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Die Funktion printf_P() unterliegt ihrer eigenen Lizenz und ist hiervon nicht betroffen
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Redistributions of source code (with or without modifications) must retain the above copyright notice,
// + this list of conditions and the following disclaimer.
// + * Neither the name of the copyright holders nor the names of contributors may be used to endorse or promote products derived
// + from this software without specific prior written permission.
// + * The use of this project (hardware, software, binary files, sources and documentation) is only permittet
// + for non-commercial use (directly or indirectly)
// + Commercial use (for excample: selling of MikroKopters, selling of PCBs, assembly, ...) is only permitted
// + with our written permission
// + * If sources or documentations are redistributet on other webpages, out webpage (http://www.MikroKopter.de) must be
// + clearly linked as origin
// + * porting to systems other than hardware from www.mikrokopter.de is not allowed
// + THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS"
// + AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE
// + IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE
// + ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE
// + LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR
// + CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF
// + SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS
// + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN// + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE)
// + ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
// + POSSIBILITY OF SUCH DAMAGE.
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
#include <stdlib.h>
#include <inttypes.h>
#include "main.h"
#include "eeprom.h"
#include "timer2.h"
#include "fc.h"
#include "rc.h"
#include "uart0.h"
#include "printf_P.h"
#include "analog.h"
#include "twimaster.h"
#ifdef USE_KILLAGREG
#include "mm3.h"
#endif
#if (defined (USE_KILLAGREG) || defined (USE_MK3MAG))
#include "ubx.h"
#endif
#if (!defined (USE_KILLAGREG) && !defined (USE_MK3MAG))
uint8_t MaxMenuItem
= 14;
#else
#ifdef USE_MK3MAG
uint8_t MaxMenuItem
= 15;
#endif
#ifdef USE_KILLAGREG
uint8_t MaxMenuItem
= 17;
#endif
#endif
uint8_t MenuItem
= 0;
uint8_t RemoteKeys
= 0;
#define KEY1 0x01
#define KEY2 0x02
#define KEY3 0x04
#define KEY4 0x08
#define KEY5 0x10
#define DISPLAYBUFFSIZE 80
int8_t DisplayBuff
[DISPLAYBUFFSIZE
] = "Hello World";
uint8_t DispPtr
= 0;
/************************************/
/* Clear LCD Buffer */
/************************************/
void LCD_Clear
(void)
{
uint8_t i
;
for( i
= 0; i
< DISPLAYBUFFSIZE
; i
++) DisplayBuff
[i
] = ' ';
}
/************************************/
/* Update Menu on LCD */
/************************************/
// Display with 20 characters in 4 lines
void LCD_PrintMenu
(void)
{
if(RemoteKeys
& KEY1
)
{
if(MenuItem
) MenuItem
--;
else MenuItem
= MaxMenuItem
;
}
if(RemoteKeys
& KEY2
)
{
if(MenuItem
== MaxMenuItem
) MenuItem
= 0;
else MenuItem
++;
}
if((RemoteKeys
& KEY1
) && (RemoteKeys
& KEY2
)) MenuItem
= 0;
LCD_Clear
();
if(MenuItem
> MaxMenuItem
) MenuItem
= MaxMenuItem
;
// print menu item number in the upper right corner
if(MenuItem
< 10)
{
LCD_printfxy
(17,0,"[%i]",MenuItem
);
}
else
{
LCD_printfxy
(16,0,"[%i]",MenuItem
);
}
switch(MenuItem
)
{
case 0:// Version Info Menu Item
LCD_printfxy
(0,0,"++ Flight-Ctrl ++");
LCD_printfxy
(0,1,"HW:V%d.%d SW:%d.%d%c",BoardRelease
/10,BoardRelease
%10,VERSION_MAJOR
, VERSION_MINOR
, VERSION_PATCH
+'a');
LCD_printfxy
(0,2,"Setting: %d %s", GetActiveParamSet
(), Mixer.
Name);
if(I2CTimeout
< 6)
{
LCD_printfxy
(0,3,"I2C Error!!!");
}
else if (MissingMotor
)
{
LCD_printfxy
(0,3,"Missing BL-Ctrl:%d", MissingMotor
);
}
else LCD_printfxy
(0,3,"(c) Holger Buss");
break;
case 1:// Height Control Menu Item
if(ParamSet.
Config0 & CFG0_AIRPRESS_SENSOR
)
{
LCD_printfxy
(0,0,"Height: %5i",(int16_t)(ReadingHeight
/5));
LCD_printfxy
(0,1,"Set Point: %5i",(int16_t)(SetPointHeight
/5));
LCD_printfxy
(0,2,"Air Press.:%5i",AdAirPressure
);
LCD_printfxy
(0,3,"Offset :%5i",OCR0A
);
}
else
{
LCD_printfxy
(0,1,"No ");
LCD_printfxy
(0,2,"Height Control");
}
break;
case 2:// Attitude Menu Item
LCD_printfxy
(0,0,"Attitude");
LCD_printfxy
(0,1,"Nick: %5i",IntegralGyroNick
/1024);
LCD_printfxy
(0,2,"Roll: %5i",IntegralGyroRoll
/1024);
LCD_printfxy
(0,3,"Heading: %5i",CompassHeading
);
break;
case 3:// Remote Control Channel Menu Item
LCD_printfxy
(0,0,"C1:%4i C2:%4i ",PPM_in
[1],PPM_in
[2]);
LCD_printfxy
(0,1,"C3:%4i C4:%4i ",PPM_in
[3],PPM_in
[4]);
LCD_printfxy
(0,2,"C5:%4i C6:%4i ",PPM_in
[5],PPM_in
[6]);
LCD_printfxy
(0,3,"C7:%4i C8:%4i ",PPM_in
[7],PPM_in
[8]);
break;
case 4:// Remote Control Mapping Menu Item
LCD_printfxy
(0,0,"Ni:%4i Ro:%4i ",PPM_in
[ParamSet.
ChannelAssignment[CH_NICK
]],PPM_in
[ParamSet.
ChannelAssignment[CH_ROLL
]]);
LCD_printfxy
(0,1,"Gs:%4i Ya:%4i ",PPM_in
[ParamSet.
ChannelAssignment[CH_GAS
]] + RC_GAS_OFFSET
,PPM_in
[ParamSet.
ChannelAssignment[CH_YAW
]]);
LCD_printfxy
(0,2,"P1:%4i P2:%4i ",PPM_in
[ParamSet.
ChannelAssignment[CH_POTI1
]] + RC_GAS_OFFSET
, PPM_in
[ParamSet.
ChannelAssignment[CH_POTI2
]] + RC_POTI_OFFSET
);
LCD_printfxy
(0,3,"P3:%4i P4:%4i ",PPM_in
[ParamSet.
ChannelAssignment[CH_POTI3
]] + RC_POTI_OFFSET
, PPM_in
[ParamSet.
ChannelAssignment[CH_POTI4
]] + RC_POTI_OFFSET
);
break;
case 5:// Gyro Sensor Menu Item
LCD_printfxy
(0,0,"Gyro - Sensor");
switch(BoardRelease
)
{
case 10:
LCD_printfxy
(0,1,"Nick %4i (%3i.%i)",AdValueGyroNick
- BiasHiResGyroNick
/ HIRES_GYRO_AMPLIFY
, BiasHiResGyroNick
/ HIRES_GYRO_AMPLIFY
, BiasHiResGyroNick
% HIRES_GYRO_AMPLIFY
);
LCD_printfxy
(0,2,"Roll %4i (%3i.%i)",AdValueGyroRoll
- BiasHiResGyroRoll
/ HIRES_GYRO_AMPLIFY
, BiasHiResGyroRoll
/ HIRES_GYRO_AMPLIFY
, BiasHiResGyroRoll
% HIRES_GYRO_AMPLIFY
);
LCD_printfxy
(0,3,"Yaw %4i (%3i)",AdBiasGyroYaw
- AdValueGyroYaw
, AdBiasGyroYaw
);
break;
case 11:
case 12:
case 20: // divice Offests by 2 becuse 2 samples are added in adc isr
LCD_printfxy
(0,1,"Nick %4i (%3i.%i)",AdValueGyroNick
- BiasHiResGyroNick
/HIRES_GYRO_AMPLIFY
, BiasHiResGyroNick
/ (HIRES_GYRO_AMPLIFY
* 2), (BiasHiResGyroNick
% (HIRES_GYRO_AMPLIFY
* 2)) / 2); // division by 2 to push the reminder below 10 (15/2 = 7)
LCD_printfxy
(0,2,"Roll %4i (%3i.%i)",AdValueGyroRoll
- BiasHiResGyroRoll
/HIRES_GYRO_AMPLIFY
, BiasHiResGyroRoll
/ (HIRES_GYRO_AMPLIFY
* 2), (BiasHiResGyroRoll
% (HIRES_GYRO_AMPLIFY
* 2)) / 2); // division by 2 to push the reminder below 10 (15/2 = 7)
LCD_printfxy
(0,3,"Yaw %4i (%3i)",AdBiasGyroYaw
- AdValueGyroYaw
, AdBiasGyroYaw
/2);
break;
case 13:
default: // divice Offests by 2 becuse 2 samples are added in adc isr
LCD_printfxy
(0,1,"Nick %4i (%3i.%i)(%3i)",AdValueGyroNick
- BiasHiResGyroNick
/HIRES_GYRO_AMPLIFY
, BiasHiResGyroNick
/ (HIRES_GYRO_AMPLIFY
* 2), (BiasHiResGyroNick
% (HIRES_GYRO_AMPLIFY
* 2))/2, DacOffsetGyroNick
); // division by 2 to push the reminder below 10 (15/2 = 7)
LCD_printfxy
(0,2,"Roll %4i (%3i.%i)(%3i)",AdValueGyroRoll
- BiasHiResGyroRoll
/HIRES_GYRO_AMPLIFY
, BiasHiResGyroRoll
/ (HIRES_GYRO_AMPLIFY
* 2), (BiasHiResGyroRoll
% (HIRES_GYRO_AMPLIFY
* 2))/2, DacOffsetGyroRoll
); // division by 2 to push the reminder below 10 (15/2 = 7)
LCD_printfxy
(0,3,"Yaw %4i (%3i)(%3i)",AdBiasGyroYaw
- AdValueGyroYaw
, AdBiasGyroYaw
/2, DacOffsetGyroYaw
);
break;
}
break;
case 6:// Acceleration Sensor Menu Item
LCD_printfxy
(0,0,"ACC - Sensor");
LCD_printfxy
(0,1,"Nick %4i (%3i)",AdValueAccNick
/2, AdBiasAccNick
/2); // factor 2 because of adding 2 samples in ADC ISR
LCD_printfxy
(0,2,"Roll %4i (%3i)",AdValueAccRoll
/2, AdBiasAccRoll
/2); // factor 2 because of adding 2 samples in ADC ISR
LCD_printfxy
(0,3,"Height %4i (%3i)",AdValueAccTop
, (int16_t)AdBiasAccTop
);
break;
case 7:// Accumulator Voltage / Remote Control Level
LCD_printfxy
(0,0,"Voltage: %3i.%1iV",UBat
/10, UBat
%10);
LCD_printfxy
(0,1,"RC-Level: %4i", RC_Quality
);
LCD_printfxy
(0,2,"RC-Channels:%4i", RC_Channels
);
LCD_printfxy
(0,3,"RC-RSSI: %4i", RC_RSSI
);
break;
case 8:// Compass Menu Item
LCD_printfxy
(0,0,"Compass ");
LCD_printfxy
(0,1,"Course: %5i",CompassCourse
);
LCD_printfxy
(0,2,"Heading: %5i",CompassHeading
);
LCD_printfxy
(0,3,"OffCourse: %5i",CompassOffCourse
);
break;
case 9:// Poti Menu Item
LCD_printfxy
(0,0,"Po1: %3i Po5: %3i" ,Poti1
,Poti5
); //PPM24-Extesion
LCD_printfxy
(0,1,"Po2: %3i Po6: %3i" ,Poti2
,Poti6
); //PPM24-Extesion
LCD_printfxy
(0,2,"Po3: %3i Po7: %3i" ,Poti3
,Poti7
); //PPM24-Extesion
LCD_printfxy
(0,3,"Po4: %3i Po8: %3i" ,Poti4
,Poti8
); //PPM24-Extesion
break;
case 10:// Servo Menu Item
LCD_printfxy
(0,0,"Servo " );
LCD_printfxy
(0,1,"Setpoint %3i",FCParam.
ServoNickControl);
LCD_printfxy
(0,2,"Position: %3i",ServoNickValue
);
LCD_printfxy
(0,3,"Range:%3i-%3i",ParamSet.
ServoNickMin, ParamSet.
ServoNickMax);
break;
case 11://Extern Control
LCD_printfxy
(0,0,"ExternControl " );
LCD_printfxy
(0,1,"Ni:%4i Ro:%4i ",ExternControl.
Nick, ExternControl.
Roll);
LCD_printfxy
(0,2,"Gs:%4i Ya:%4i ",ExternControl.
Gas, ExternControl.
Yaw);
LCD_printfxy
(0,3,"Hi:%4i Cf:%4i ",ExternControl.
Height, ExternControl.
Config);
break;
case 12://BL Communication errors
LCD_printfxy
(0,0,"BL-Ctrl Errors " );
LCD_printfxy
(0,1," %3d %3d %3d %3d ",Motor
[0].
Error,Motor
[1].
Error,Motor
[2].
Error,Motor
[3].
Error);
LCD_printfxy
(0,2," %3d %3d %3d %3d ",Motor
[4].
Error,Motor
[5].
Error,Motor
[6].
Error,Motor
[7].
Error);
LCD_printfxy
(0,3," %3d %3d %3d %3d ",Motor
[8].
Error,Motor
[9].
Error,Motor
[10].
Error,Motor
[11].
Error);
break;
case 13://BL Overview
LCD_printfxy
(0,0,"BL-Ctrl found " );
LCD_printfxy
(0,1," %c %c %c %c ",Motor
[0].
Present + '-',Motor
[1].
Present + '-',Motor
[2].
Present + '-',Motor
[3].
Present + '-');
LCD_printfxy
(0,2," %c %c %c %c ",Motor
[4].
Present + '-',Motor
[5].
Present + '-',Motor
[6].
Present + '-',Motor
[7].
Present + '-');
LCD_printfxy
(0,3," %c - - - ",Motor
[8].
Present + '-');
if(Motor
[9].
Present) LCD_printfxy
(4,3,"10");
if(Motor
[10].
Present) LCD_printfxy
(8,3,"11");
if(Motor
[11].
Present) LCD_printfxy
(12,3,"12");
break;
case 14:// flight time counter
LCD_printfxy
(0,0,"Flight-Time " );
LCD_printfxy
(0,1,"Trip: %5u min",FlightMinutes
);
LCD_printfxy
(0,2,"Total:%5u min",FlightMinutesTotal
);
LCD_printfxy
(13,3,"(reset)");
if(RemoteKeys
& KEY4
)
{
FlightMinutes
= 0;
SetParamWord
(PID_FLIGHT_MINUTES
, FlightMinutes
);
}
break;
#if (defined (USE_KILLAGREG) || defined (USE_MK3MAG))
case 15://GPS Lat/Lon coords
if (GPSInfo.
status == INVALID
)
{
LCD_printfxy
(0,0,"No GPS data!");
}
else
{
switch (GPSInfo.
satfix)
{
case SATFIX_NONE
:
LCD_printfxy
(0,0,"Sats: %d Fix: No", GPSInfo.
satnum);
break;
case SATFIX_2D
:
LCD_printfxy
(0,0,"Sats: %d Fix: 2D", GPSInfo.
satnum);
break;
case SATFIX_3D
:
LCD_printfxy
(0,0,"Sats: %d Fix: 3D", GPSInfo.
satnum);
break;
default:
LCD_printfxy
(0,0,"Sats: %d Fix: ??", GPSInfo.
satnum);
break;
}
int16_t i1
,i2
,i3
;
i1
= (int16_t)(GPSInfo.
longitude/10000000L);
i2
= abs((int16_t)((GPSInfo.
longitude%10000000L
)/10000L));
i3
= abs((int16_t)(((GPSInfo.
longitude%10000000L
)%10000L
)/10L));
LCD_printfxy
(0,1,"Lon: %d.%03d%03d deg",i1
, i2
, i3
);
i1
= (int16_t)(GPSInfo.
latitude/10000000L);
i2
= abs((int16_t)((GPSInfo.
latitude%10000000L
)/10000L));
i3
= abs((int16_t)(((GPSInfo.
latitude%10000000L
)%10000L
)/10L));
LCD_printfxy
(0,2,"Lat: %d.%03d%03d deg",i1
, i2
, i3
);
i1
= (int16_t)(GPSInfo.
altitude/1000L);
i2
= abs((int16_t)(GPSInfo.
altitude%1000L
));
LCD_printfxy
(0,3,"Alt: %d.%03d m",i1
, i2
);
}
break;
#endif
#ifdef USE_KILLAGREG
case 16:// MM3 Kompass
LCD_printfxy
(0,0,"MM3 Offset");
LCD_printfxy
(0,1,"X_Offset: %3i",MM3_calib.
X_off);
LCD_printfxy
(0,2,"Y_Offset: %3i",MM3_calib.
Y_off);
LCD_printfxy
(0,3,"Z_Offset: %3i",MM3_calib.
Z_off);
break;
case 17://MM3 Range
LCD_printfxy
(0,0,"MM3 Range");
LCD_printfxy
(0,1,"X_Range: %4i",MM3_calib.
X_range);
LCD_printfxy
(0,2,"Y_Range: %4i",MM3_calib.
Y_range);
LCD_printfxy
(0,3,"Z_Range: %4i",MM3_calib.
Z_range);
break;
#endif
default:
MaxMenuItem
= MenuItem
- 1;
MenuItem
= 0;
break;
}
RemoteKeys
= 0;
}