Rev 2041 |
Blame |
Last modification |
View Log
| RSS feed
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Copyright (c) 04.2007 Holger Buss
// + Nur f�r den privaten Gebrauch
// + www.MikroKopter.com
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Es gilt f�r das gesamte Projekt (Hardware, Software, Bin�rfiles, Sourcecode und Dokumentation),
// + dass eine Nutzung (auch auszugsweise) nur f�r den privaten (nicht-kommerziellen) Gebrauch zul�ssig 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, Best�ckung und Verkauf von Platinen oder Baus�tzen,
// + Verkauf von Luftbildaufnahmen, usw.
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder ver�ffentlicht,
// + unterliegen sie auch diesen Nutzungsbedingungen und diese Nutzungsbedingungen incl. Copyright m�ssen dann beiliegen
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts
// + auf anderen Webseiten oder sonstigen Medien ver�ffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de"
// + eindeutig als Ursprung verlinkt werden
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Keine Gew�hr auf Fehlerfreiheit, Vollst�ndigkeit oder Funktion
// + Benutzung auf eigene Gefahr
// + Wir �bernehmen keinerlei Haftung f�r direkte oder indirekte Personen- oder Sachsch�den
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Die Portierung der Software (oder Teile davon) auf andere Systeme (ausser der Hardware von www.mikrokopter.de) ist nur
// + mit unserer Zustimmung zul�ssig
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + 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 example: 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 "eeprom.h"
#include "timer2.h"
#include "rc.h"
#include "externalControl.h"
#include "uart0.h"
#include "printf_P.h"
#include "analog.h"
#include "twimaster.h"
#include "attitude.h"
#if (!defined (USE_NAVICTRL))
uint8_t maxMenuItem
= 13;
#else
#ifdef USE_NAVICTRL
#include "gps.c"
uint8_t maxMenuItem
= 14;
#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, "+ MikroKopter +");
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
(), mixerMatrix.
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(staticParams.GlobalConfig & CFG_HEIGHT_CONTROL) {
LCD_printfxy(0,0,"Height: %5i",ReadingHeight);
LCD_printfxy(0,1,"Set Point: %5i",SetPointHeight);
LCD_printfxy(0,2,"Air Press.:%5i",0);
LCD_printfxy(0,3,"Offset :%5i",0);
}
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",
attitude
[PITCH
] / GYRO_DEG_FACTOR_PITCHROLL
);
LCD_printfxy
(0, 2, "Roll: %5i",
attitude
[ROLL
] / GYRO_DEG_FACTOR_PITCHROLL
);
LCD_printfxy
(0, 3, "Heading(M):%5i", magneticHeading
);
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
[channelMap.
channels[CH_PITCH
]], PPM_in
[channelMap.
channels[CH_ROLL
]]);
LCD_printfxy
(
0,
1,
"Gs:%4i Ya:%4i ",
PPM_in
[channelMap.
channels[CH_THROTTLE
]], PPM_in
[channelMap.
channels[CH_YAW
]]);
LCD_printfxy
(
0,
2,
"P1:%4i P2:%4i ",
PPM_in
[channelMap.
channels[CH_POTS
]], PPM_in
[channelMap.
channels[CH_POTS
+1]]);
LCD_printfxy
(
0,
3,
"P3:%4i P4:%4i ",
PPM_in
[channelMap.
channels[CH_POTS
+2]], PPM_in
[channelMap.
channels[CH_POTS
+3]]);
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 - HiResNickOffset / HIRES_GYRO_AMPLIFY, HiResNickOffset / HIRES_GYRO_AMPLIFY, HiResNickOffset % HIRES_GYRO_AMPLIFY);
LCD_printfxy(0,2,"Roll %4i (%3i.%i)", AdValueGyroRoll - HiResRollOffset / HIRES_GYRO_AMPLIFY, HiResRollOffset / HIRES_GYRO_AMPLIFY, HiResRollOffset % HIRES_GYRO_AMPLIFY);
LCD_printfxy(0,3,"Yaw %4i (%3i)", AdValueGyroYaw , YawOffset);
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)",0, HiResNickOffset / (HIRES_GYRO_AMPLIFY * 2), (HiResNickOffset % (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)",0, HiResRollOffset / (HIRES_GYRO_AMPLIFY * 2), (HiResRollOffset % (HIRES_GYRO_AMPLIFY * 2)) / 2); // division by 2 to push the reminder below 10 (15/2 = 7)
LCD_printfxy(0,3,"Yaw %4i (%3i)",YawOffset - AdValueGyroYaw , YawOffset/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)",0, HiResNickOffset / (HIRES_GYRO_AMPLIFY * 2), (HiResNickOffset % (HIRES_GYRO_AMPLIFY * 2))/2, 0); // division by 2 to push the reminder below 10 (15/2 = 7)
LCD_printfxy(0,2,"Roll %4i (%3i.%i)(%3i)",0, HiResRollOffset / (HIRES_GYRO_AMPLIFY * 2), (HiResRollOffset % (HIRES_GYRO_AMPLIFY * 2))/2, 0); // division by 2 to push the reminder below 10 (15/2 = 7)
LCD_printfxy(0,3,"Yaw %4i (%3i)(%3i)",YawOffset - AdValueGyroYaw , YawOffset/2, 0);
break;
}
break;
case 6:// Acceleration Sensor Menu Item
LCD_printfxy(0,0,"ACC - Sensor");
LCD_printfxy(0,1,"Nick %4i (%3i)",0,0); // factor 2 because of adding 2 samples in ADC ISR
LCD_printfxy(0,2,"Roll %4i (%3i)",0,0); // factor 2 because of adding 2 samples in ADC ISR
LCD_printfxy(0,3,"Height %4i (%3i)",0,0);
break;
*/
case 7: // Battery Voltage / Remote Control Level
LCD_printfxy
(0, 1, "Voltage: %3i.%1iV", UBat
/10, UBat
%10);
LCD_printfxy
(0, 2, "RC-Level: %5i", RCQuality
);
break;
case 8: // Compass Menu Item
LCD_printfxy
(0, 0, "Compass ");
LCD_printfxy
(0, 0, "TODO: Impl. ");
break;
case 9: // Poti Menu Item
LCD_printfxy
(0, 0, "Variables ");
LCD_printfxy
(0, 0, "TODO: Impl. ");
break;
case 10: // Servo Menu Item
LCD_printfxy
(0, 0, "Servos ");
LCD_printfxy
(0, 0, "TODO: Impl. ");
break;
case 11: //Extern Control
LCD_printfxy
(0, 0, "ExternControl ");
LCD_printfxy
(0, 1, "Ni:%4i Ro:%4i ",
externalControl.
pitch, externalControl.
roll);
LCD_printfxy
(0, 2, "Gs:%4i Ya:%4i ",
externalControl.
throttle, externalControl.
yaw);
LCD_printfxy
(0, 3, "Hi:%4i Cf:%4i ",
externalControl.
height, externalControl.
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;
#if (defined (USE_NAVICTRL))
case 14: //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
default:
maxMenuItem
= menuItem
- 1;
menuItem
= 0;
break;
}
remoteKeys
= 0;
}