WebSVN - FlightCtrl - Diff - Rev 898 and 2147 - /branches/V0.68d CRK HexaLotte/fc.c


/*#######################################################################################
Flight Control
#######################################################################################*/
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Copyright (c) 04.2007 Holger Buss
// + Nur für den privaten Gebrauch
// + www.MikroKopter.com
//Ê²Ã´ÒÀÏ¡
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + 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 <avr/io.h>
 
#include "main.h"
#include "eeprom.h"
#include "timer0.h"
#include "_Settings.h"
#include "analog.h"
#include "fc.h"
#include "gps.h"
#include "uart.h"
#include "rc.h"
#include "twimaster.h"
#ifdef USE_MM3
#include "mm3.h"
#endif
#ifdef USE_CMPS03
#include "cmps03.h"
#endif
#include "led.h"
 
volatile uint16_t I2CTimeout = 100;
// gyro readings
volatile int16_t Reading_GyroPitch, Reading_GyroRoll, Reading_GyroYaw;
// gyro neutral readings
volatile int16_t AdNeutralPitch = 0, AdNeutralRoll = 0, AdNeutralYaw = 0;
volatile int16_t StartNeutralRoll = 0, StartNeutralPitch = 0;
// mean accelerations
volatile int16_t Mean_AccPitch, Mean_AccRoll, Mean_AccTop;
 
// neutral acceleration readings
volatile int16_t NeutralAccX=0, NeutralAccY=0;
volatile float NeutralAccZ = 0;
 
// attitude gyro integrals
volatile int32_t IntegralPitch = 0,IntegralPitch2 = 0;
volatile int32_t IntegralRoll = 0,IntegralRoll2 = 0;
volatile int32_t IntegralYaw = 0;
volatile int32_t Reading_IntegralGyroPitch = 0, Reading_IntegralGyroPitch2 = 0;
volatile int32_t Reading_IntegralGyroRoll = 0,  Reading_IntegralGyroRoll2 = 0;
volatile int32_t Reading_IntegralGyroYaw = 0;
volatile int32_t MeanIntegralPitch;
volatile int32_t MeanIntegralRoll;
 
// attitude acceleration integrals
volatile int32_t IntegralAccPitch = 0, IntegralAccRoll = 0;
volatile int32_t Reading_Integral_Top = 0;
 
// compass course
volatile int16_t CompassHeading = -1; // negative angle indicates invalid data.
volatile int16_t CompassCourse = -1;
volatile int16_t CompassOffCourse = 0;
 
// flags
uint8_t MotorsOn = 0;
uint8_t EmergencyLanding = 0;
 
int32_t TurnOver180Pitch = 250000L, TurnOver180Roll = 250000L;
 
float Gyro_P_Factor;
float Gyro_I_Factor;
 
volatile int16_t  DiffPitch, DiffRoll;
 
int16_t  Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0, Poti5 = 0, Poti6 = 0, Poti7 = 0, Poti8 = 0;
 
// setpoints for motors
volatile uint8_t Motor_FrontLeft, Motor_FrontRight, Motor_RearLeft, Motor_RearRight, Motor_Right, Motor_Left;
 
// stick values derived by rc channels readings
int16_t StickPitch = 0, StickRoll = 0, StickYaw = 0, StickThrust = 0;
int16_t MaxStickPitch = 0, MaxStickRoll = 0;
// stick values derived by uart inputs
int16_t ExternStickPitch = 0, ExternStickRoll = 0, ExternStickYaw = 0, ExternHeightValue = -20;
 
 
 
 
int16_t ReadingHeight = 0;
int16_t SetPointHeight = 0;
 
int16_t AttitudeCorrectionRoll = 0, AttitudeCorrectionPitch = 0;
 
float Ki =  FACTOR_I;
 
uint8_t Looping_Pitch = 0, Looping_Roll = 0;
uint8_t Looping_Left = 0, Looping_Right = 0, Looping_Down = 0, Looping_Top = 0;
 
 
fc_param_t FCParam = {48,251,16,58,64,150,150,2,10,0,0,0,0,0,0,0,0,100,70,0,0,100};
 
 
/************************************************************************/
/*  Creates numbeeps beeps at the speaker                               */
/************************************************************************/
void Beep(uint8_t numbeeps)
{
        while(numbeeps--)
        {
                if(MotorsOn) return; //auf keinen Fall im Flug!
                BeepTime = 100; // 0.1 second
                Delay_ms(250); // blocks 250 ms as pause to next beep,
                // this will block the flight control loop,
                // therefore do not use this funktion if motors are running
        }
}
 
/************************************************************************/
/*  Neutral Readings                                                    */
/************************************************************************/
void SetNeutral(void)
{
        NeutralAccX = 0;
        NeutralAccY = 0;
        NeutralAccZ = 0;
    AdNeutralPitch = 0;
        AdNeutralRoll = 0;
        AdNeutralYaw = 0;
    FCParam.Yaw_PosFeedback = 0;
    FCParam.Yaw_NegFeedback = 0;
    CalibMean();
    Delay_ms_Mess(100);
        CalibMean();
    if((ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL))  // Height Control activated?
    {
                if((ReadingAirPressure > 950) || (ReadingAirPressure < 750)) SearchAirPressureOffset();
    }
        AdNeutralPitch = AdValueGyrPitch;
        AdNeutralRoll  = AdValueGyrRoll;
        AdNeutralYaw   = AdValueGyrYaw;
        StartNeutralRoll  = AdNeutralRoll;
        StartNeutralPitch = AdNeutralPitch;
    if(GetParamWord(PID_ACC_PITCH) > 1023)
    {
                NeutralAccY = abs(Mean_AccRoll) / ACC_AMPLIFY;
                NeutralAccX = abs(Mean_AccPitch) / ACC_AMPLIFY;
                NeutralAccZ = Current_AccZ;
    }
    else
    {
                NeutralAccX = (int16_t)GetParamWord(PID_ACC_PITCH);
            NeutralAccY = (int16_t)GetParamWord(PID_ACC_ROLL);
            NeutralAccZ = (int16_t)GetParamWord(PID_ACC_Z);
    }
        Reading_IntegralGyroPitch = 0;
    Reading_IntegralGyroPitch2 = 0;
    Reading_IntegralGyroRoll = 0;
    Reading_IntegralGyroRoll2 = 0;
    Reading_IntegralGyroYaw = 0;
    Reading_GyroPitch = 0;
    Reading_GyroRoll = 0;
    Reading_GyroYaw = 0;
    StartAirPressure = AirPressure;
    HeightD = 0;
    Reading_Integral_Top = 0;
    CompassCourse = CompassHeading;
    BeepTime = 50;
        TurnOver180Pitch = (int32_t) ParamSet.AngleTurnOverPitch * 2500L;
        TurnOver180Roll = (int32_t) ParamSet.AngleTurnOverRoll * 2500L;
    ExternHeightValue = 0;
    GPS_Neutral();
}
 
/************************************************************************/
/*  Averaging Measurement Readings                                      */
/************************************************************************/
void Mean(void)
{
    static int32_t tmpl,tmpl2;
 
 // Get offset corrected gyro readings (~ to angular velocity)
    Reading_GyroYaw   = AdNeutralYaw    - AdValueGyrYaw;
    Reading_GyroRoll  = AdValueGyrRoll  - AdNeutralRoll;
    Reading_GyroPitch = AdValueGyrPitch - AdNeutralPitch;
 
        DebugOut.Analog[26] = Reading_GyroPitch;
        DebugOut.Analog[28] = Reading_GyroRoll;
 
// Acceleration Sensor
        // sliding average sensor readings
        Mean_AccPitch = ((int32_t)Mean_AccPitch * 1 + ((ACC_AMPLIFY * (int32_t)AdValueAccPitch))) / 2L;
        Mean_AccRoll  = ((int32_t)Mean_AccRoll * 1 + ((ACC_AMPLIFY * (int32_t)AdValueAccRoll))) / 2L;
        Mean_AccTop   = ((int32_t)Mean_AccTop * 1 + ((int32_t)AdValueAccTop)) / 2L;
 
        // sum sensor readings for later averaging
    IntegralAccPitch += ACC_AMPLIFY * AdValueAccPitch;
    IntegralAccRoll  += ACC_AMPLIFY * AdValueAccRoll;
 
// Yaw
        // calculate yaw gyro intergral (~ to rotation angle)
    Reading_IntegralGyroYaw  += Reading_GyroYaw;
        // Coupling fraction
        if(!Looping_Pitch && !Looping_Roll && (ParamSet.GlobalConfig & CFG_AXIS_COUPLING_ACTIVE))
        {
                tmpl = Reading_IntegralGyroPitch / 4096L;
                tmpl *= Reading_GyroYaw;
                tmpl *= FCParam.Yaw_PosFeedback;  //125
                tmpl /= 2048L;
                tmpl2 = Reading_IntegralGyroRoll / 4096L;
                tmpl2 *= Reading_GyroYaw;
                tmpl2 *= FCParam.Yaw_PosFeedback;
                tmpl2 /= 2048L;
        }
        else  tmpl = tmpl2 = 0;
 
// Roll
        Reading_GyroRoll += tmpl;
        Reading_GyroRoll += (tmpl2 * FCParam.Yaw_NegFeedback) / 512L;
        Reading_IntegralGyroRoll2 += Reading_GyroRoll;
        Reading_IntegralGyroRoll +=  Reading_GyroRoll - AttitudeCorrectionRoll;
        if(Reading_IntegralGyroRoll > TurnOver180Roll)
        {
                Reading_IntegralGyroRoll  = -(TurnOver180Roll - 10000L);
                Reading_IntegralGyroRoll2 = Reading_IntegralGyroRoll;
        }
        if(Reading_IntegralGyroRoll < -TurnOver180Roll)
        {
                Reading_IntegralGyroRoll =  (TurnOver180Roll - 10000L);
                Reading_IntegralGyroRoll2 = Reading_IntegralGyroRoll;
        }
        if(AdValueGyrRoll < 15)   Reading_GyroRoll = -1000;
        if(AdValueGyrRoll <  7)   Reading_GyroRoll = -2000;
        if(BoardRelease == 10)
        {
                if(AdValueGyrRoll > 1010) Reading_GyroRoll = +1000;
                if(AdValueGyrRoll > 1017) Reading_GyroRoll = +2000;
        }
        else
        {
                if(AdValueGyrRoll > 2020) Reading_GyroRoll = +1000;
                if(AdValueGyrRoll > 2034) Reading_GyroRoll = +2000;
        }
// Pitch
        Reading_GyroPitch -= tmpl2;
        Reading_GyroPitch -= (tmpl*FCParam.Yaw_NegFeedback) / 512L;
        Reading_IntegralGyroPitch2 += Reading_GyroPitch;
        Reading_IntegralGyroPitch  += Reading_GyroPitch - AttitudeCorrectionPitch;
        if(Reading_IntegralGyroPitch > TurnOver180Pitch)
        {
         Reading_IntegralGyroPitch = -(TurnOver180Pitch - 10000L);
         Reading_IntegralGyroPitch2 = Reading_IntegralGyroPitch;
        }
        if(Reading_IntegralGyroPitch < -TurnOver180Pitch)
        {
         Reading_IntegralGyroPitch =  (TurnOver180Pitch - 10000L);
         Reading_IntegralGyroPitch2 = Reading_IntegralGyroPitch;
        }
        if(AdValueGyrPitch < 15)   Reading_GyroPitch = -1000;
        if(AdValueGyrPitch <  7)   Reading_GyroPitch = -2000;
        if(BoardRelease == 10)
        {
                if(AdValueGyrPitch > 1010) Reading_GyroPitch = +1000;
                if(AdValueGyrPitch > 1017) Reading_GyroPitch = +2000;
        }
        else
        {
                if(AdValueGyrPitch > 2020) Reading_GyroPitch = +1000;
                if(AdValueGyrPitch > 2034) Reading_GyroPitch = +2000;
        }
 
// start ADC again to capture measurement values for the next loop
    ADC_Enable();
 
    IntegralYaw    = Reading_IntegralGyroYaw;
    IntegralPitch  = Reading_IntegralGyroPitch;
    IntegralRoll   = Reading_IntegralGyroRoll;
    IntegralPitch2 = Reading_IntegralGyroPitch2;
    IntegralRoll2  = Reading_IntegralGyroRoll2;
 
        if((ParamSet.GlobalConfig & CFG_ROTARY_RATE_LIMITER) && !Looping_Pitch && !Looping_Roll)
        {
                if(Reading_GyroPitch > 200)       Reading_GyroPitch += 4 * (Reading_GyroPitch - 200);
                else if(Reading_GyroPitch < -200) Reading_GyroPitch += 4 * (Reading_GyroPitch + 200);
                if(Reading_GyroRoll > 200)        Reading_GyroRoll  += 4 * (Reading_GyroRoll - 200);
                else if(Reading_GyroRoll < -200)  Reading_GyroRoll  += 4 * (Reading_GyroRoll + 200);
        }
}
 
/************************************************************************/
/*  Averaging Measurement Readings  for Calibration                     */
/************************************************************************/
void CalibMean(void)
{
    // stop ADC to avoid changing values during calculation
        ADC_Disable();
 
        Reading_GyroPitch = AdValueGyrPitch;
        Reading_GyroRoll  = AdValueGyrRoll;
        Reading_GyroYaw   = AdValueGyrYaw;
 
        Mean_AccPitch = ACC_AMPLIFY * (int32_t)AdValueAccPitch;
        Mean_AccRoll  = ACC_AMPLIFY * (int32_t)AdValueAccRoll;
        Mean_AccTop   = (int32_t)AdValueAccTop;
    // start ADC (enables internal trigger so that the ISR in analog.c
    // updates the readings once)
    ADC_Enable();
 
        TurnOver180Pitch = (int32_t) ParamSet.AngleTurnOverPitch * 2500L;
        TurnOver180Roll =  (int32_t) ParamSet.AngleTurnOverRoll  * 2500L;
}
 
/************************************************************************/
/*  Transmit Motor Data via I2C                                         */
/************************************************************************/
void SendMotorData(void)
{
    if(MOTOR_OFF || !MotorsOn)
    {
        Motor_RearLeft = 0;
                Motor_RearRight = 0;
        Motor_FrontLeft = 0;
                Motor_FrontRight = 0;
        Motor_Right = 0;
        Motor_Left = 0;
        if(MotorTest[0]) Motor_FrontLeft = Motor_FrontRight = MotorTest[0];
        if(MotorTest[1]) Motor_RearLeft  = Motor_RearRight  = MotorTest[1];
        if(MotorTest[2]) Motor_Left  = MotorTest[2];
        if(MotorTest[3]) Motor_Right = MotorTest[3];
     }
 
    DebugOut.Analog[12] = Motor_FrontLeft;
    DebugOut.Analog[13] = Motor_RearRight;
    DebugOut.Analog[14] = Motor_FrontRight;
    DebugOut.Analog[15] = Motor_RearLeft;
    DebugOut.Analog[16] = Motor_Left;
    DebugOut.Analog[17] = Motor_Right;
       
    //Start I2C Interrupt Mode
    twi_state = 0;
    motor = 0;
    I2C_Start();
}
 
 
 
/************************************************************************/
/*  Maps the parameter to poti values                                   */
/************************************************************************/
void ParameterMapping(void)
{
        if(RC_Quality > 160) // do the mapping of RC-Potis only if the rc-signal is ok
        // else the last updated values are used
        {
                 //update poti values by rc-signals
                #define CHK_POTI(b,a,min,max) { if(a > 250) { if(a == 251) b = Poti1; else if(a == 252) b = Poti2; else if(a == 253) b = Poti3; else if(a == 254) b = Poti4;} else b = a; if(b <= min) b = min; else if(b >= max) b = max;}
                CHK_POTI(FCParam.MaxHeight,ParamSet.MaxHeight,0,255);
                CHK_POTI(FCParam.Height_D,ParamSet.Height_D,0,100);
                CHK_POTI(FCParam.Height_P,ParamSet.Height_P,0,100);
                CHK_POTI(FCParam.Height_ACC_Effect,ParamSet.Height_ACC_Effect,0,255);
                CHK_POTI(FCParam.CompassYawEffect,ParamSet.CompassYawEffect,0,255);
                CHK_POTI(FCParam.Gyro_P,ParamSet.Gyro_P,10,255);
                CHK_POTI(FCParam.Gyro_I,ParamSet.Gyro_I,0,255);
                CHK_POTI(FCParam.I_Factor,ParamSet.I_Factor,0,255);
                CHK_POTI(FCParam.UserParam1,ParamSet.UserParam1,0,255);
                CHK_POTI(FCParam.UserParam2,ParamSet.UserParam2,0,255);
                CHK_POTI(FCParam.UserParam3,ParamSet.UserParam3,0,255);
                CHK_POTI(FCParam.UserParam4,ParamSet.UserParam4,0,255);
                CHK_POTI(FCParam.UserParam5,ParamSet.UserParam5,0,255);
                CHK_POTI(FCParam.UserParam6,ParamSet.UserParam6,0,255);
                CHK_POTI(FCParam.UserParam7,ParamSet.UserParam7,0,255);
                CHK_POTI(FCParam.UserParam8,ParamSet.UserParam8,0,255);
                CHK_POTI(FCParam.ServoPitchControl,ParamSet.ServoPitchControl,0,255);
                CHK_POTI(FCParam.LoopThrustLimit,ParamSet.LoopThrustLimit,0,255);
                CHK_POTI(FCParam.Yaw_PosFeedback,ParamSet.Yaw_PosFeedback,0,255);
                CHK_POTI(FCParam.Yaw_NegFeedback,ParamSet.Yaw_NegFeedback,0,255);
                CHK_POTI(FCParam.DynamicStability,ParamSet.DynamicStability,0,255);
                Ki = (float) FCParam.I_Factor * FACTOR_I;
        }
}
 
 
/************************************************************************/
/*  MotorControl                                                        */
/************************************************************************/
void MotorControl(void)
{
        int16_t MotorValue, pd_result, h, tmp_int;
        int16_t YawMixFraction, ThrustMixFraction, PitchMixFraction, RollMixFraction;
        static int32_t SumPitch = 0, SumRoll = 0;
        static int32_t SetPointYaw = 0;
        static int32_t IntegralErrorPitch = 0;
        static int32_t IntegralErrorRoll = 0;
        static uint16_t RcLostTimer;
        static uint8_t delay_neutral = 0, delay_startmotors = 0, delay_stopmotors = 0;
        static uint16_t Model_Is_Flying = 0;
        static uint8_t HeightControlActive = 0;
        static int16_t HeightControlThrust = 0;
        static int8_t TimerDebugOut = 0;
        static uint16_t UpdateCompassCourse = 0;
        static int32_t CorrectionPitch, CorrectionRoll;
 
        Mean();
        GRN_ON;
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// determine thrust value
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        ThrustMixFraction = StickThrust;
    if(ThrustMixFraction < 0) ThrustMixFraction = 0;
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// RC-signal is bad
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        if(RC_Quality < 120)  // the rc-frame signal is not reveived or noisy
        {
                if(!PcAccess) // if also no PC-Access via UART
                {
                        if(BeepModulation == 0xFFFF)
                        {
                         BeepTime = 15000; // 1.5 seconds
                         BeepModulation = 0x0C00;
                        }
                }
                if(RcLostTimer) RcLostTimer--; // decremtent timer after rc sigal lost
                else // rc lost countdown finished
                {
                  MotorsOn = 0; // stop all motors
                  EmergencyLanding = 0; // emergency landing is over
                }
                ROT_ON; // set red led
                if(Model_Is_Flying > 2000)  // wahrscheinlich in der Luft --> langsam absenken
                {
                        ThrustMixFraction = ParamSet.EmergencyThrust; // set emergency thrust
                        EmergencyLanding = 1; // enable emergency landing
                        // set neutral rc inputs
                        PPM_diff[ParamSet.ChannelAssignment[CH_PITCH]] = 0;
                        PPM_diff[ParamSet.ChannelAssignment[CH_ROLL]] = 0;
                        PPM_diff[ParamSet.ChannelAssignment[CH_YAW]] = 0;
                        PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] = 0;
                        PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] = 0;
                        PPM_in[ParamSet.ChannelAssignment[CH_YAW]] = 0;
                }
                else MotorsOn = 0; // switch of all motors
        } // eof RC_Quality < 120
        else
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// RC-signal is good
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        if(RC_Quality > 150)
        {
                EmergencyLanding = 0; // switch off emergency landing if RC-signal is okay
                // reset emergency timer
                RcLostTimer = ParamSet.EmergencyThrustDuration * 50;
                if(ThrustMixFraction > 40)
                {
                        if(Model_Is_Flying < 0xFFFF) Model_Is_Flying++;
                }
                if((Model_Is_Flying < 200) || (ThrustMixFraction < 40))
                {
                        SumPitch = 0;
                        SumRoll = 0;
                        Reading_IntegralGyroYaw = 0;
                }
 
                if(Poti1 < PPM_in[ParamSet.ChannelAssignment[CH_POTI1]] + 110) Poti1++; else if(Poti1 > PPM_in[ParamSet.ChannelAssignment[CH_POTI1]] + 110 && Poti1) Poti1--;
                if(Poti2 < PPM_in[ParamSet.ChannelAssignment[CH_POTI2]] + 110) Poti2++; else if(Poti2 > PPM_in[ParamSet.ChannelAssignment[CH_POTI2]] + 110 && Poti2) Poti2--;
                if(Poti3 < PPM_in[ParamSet.ChannelAssignment[CH_POTI3]] + 110) Poti3++; else if(Poti3 > PPM_in[ParamSet.ChannelAssignment[CH_POTI3]] + 110 && Poti3) Poti3--;
                if(Poti4 < PPM_in[ParamSet.ChannelAssignment[CH_POTI4]] + 110) Poti4++; else if(Poti4 > PPM_in[ParamSet.ChannelAssignment[CH_POTI4]] + 110 && Poti4) Poti4--;
                //PPM24-Extension
                if(Poti5 < PPM_in[9] + 110)  Poti5++; else if(Poti5 >  PPM_in[9] + 110 && Poti5) Poti5--;
                if(Poti6 < PPM_in[10] + 110) Poti6++; else if(Poti6 > PPM_in[10] + 110 && Poti6) Poti6--;
                if(Poti7 < PPM_in[11] + 110) Poti7++; else if(Poti7 > PPM_in[11] + 110 && Poti7) Poti7--;
                if(Poti8 < PPM_in[12] + 110) Poti8++; else if(Poti8 > PPM_in[12] + 110 && Poti8) Poti8--;
                //limit poti values
                if(Poti1 < 0) Poti1 = 0; else if(Poti1 > 255) Poti1 = 255;
                if(Poti2 < 0) Poti2 = 0; else if(Poti2 > 255) Poti2 = 255;
                if(Poti3 < 0) Poti3 = 0; else if(Poti3 > 255) Poti3 = 255;
                if(Poti4 < 0) Poti4 = 0; else if(Poti4 > 255) Poti4 = 255;
                //PPM24-Extension
                if(Poti5 < 0) Poti5 = 0; else if(Poti5 > 255) Poti5 = 255;
                if(Poti6 < 0) Poti6 = 0; else if(Poti6 > 255) Poti6 = 255;
                if(Poti7 < 0) Poti7 = 0; else if(Poti7 > 255) Poti7 = 255;
                if(Poti8 < 0) Poti8 = 0; else if(Poti8 > 255) Poti8 = 255;
 
                // if motors are off and the thrust stick is in the upper position
                if((PPM_in[ParamSet.ChannelAssignment[CH_THRUST]] > 80) && MotorsOn == 0)
                {
                        // and if the yaw stick is in the leftmost position
                        if(PPM_in[ParamSet.ChannelAssignment[CH_YAW]] > 75)
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// calibrate the neutral readings of all attitude sensors
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
                        {
                                if(++delay_neutral > 200)  // not immediately (wait 200 loops = 200 * 2ms = 0.4 s)
                                {
                                        delay_neutral = 0;
                                        GRN_OFF;
                                        Model_Is_Flying = 0;
                                        // check roll/pitch stick position
                                        // if pitch stick is topmost or roll stick is leftmost --> change parameter setting
                                        // according to roll/pitch stick position
                                        if(PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] > 70 || abs(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]]) > 70)
                                        {
                                                 uint8_t setting = 1; // default
                                                 //  _________
                                                 // |2   3   4|
                                                 // |         |
                                                 // |1       5|
                                                 // |         |
                                                 // |_________|
                                                 //
                                                 // roll stick leftmost and pitch stick centered --> setting 1
                                                 if(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] > 70 && PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] < 70) setting = 1;
                                                 // roll stick leftmost and pitch stick topmost --> setting 2
                                                 if(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] > 70 && PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] > 70) setting = 2;
                                                 // roll stick centered an pitch stick topmost --> setting 3
                                                 if(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] < 70 && PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] > 70) setting = 3;
                                                 // roll stick rightmost and pitch stick topmost --> setting 4
                                                 if(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] <-70 && PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] > 70) setting = 4;
                                                 // roll stick rightmost and pitch stick centered --> setting 5
                                                 if(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] <-70 && PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] < 70) setting = 5;
                                                 // update active parameter set in eeprom
                                                 SetActiveParamSet(setting);
                                        }
                                        ParamSet_ReadFromEEProm(GetActiveParamSet());
                                        SetNeutral();
                                        Beep(GetActiveParamSet());
                                }
                        }
                        // and if the yaw stick is in the rightmost position
                        // save the ACC neutral setting to eeprom
                        else if(PPM_in[ParamSet.ChannelAssignment[CH_YAW]] < -75)
                        {
                                if(++delay_neutral > 200)  // not immediately (wait 200 loops = 200 * 2ms = 0.4 s)
                                {
                                        delay_neutral = 0;
                                        GRN_OFF;
                                        SetParamWord(PID_ACC_PITCH, 0xFFFF); // make value invalid
                                        Model_Is_Flying = 0;
                                        SetNeutral();
                                        // Save ACC neutral settings to eeprom
                                        SetParamWord(PID_ACC_PITCH, (uint16_t)NeutralAccX);
                                        SetParamWord(PID_ACC_ROLL,  (uint16_t)NeutralAccY);
                                        SetParamWord(PID_ACC_Z,     (uint16_t)NeutralAccZ);
                                        Beep(GetActiveParamSet());
                                }
                        }
                        else delay_neutral = 0;
                }
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// thrust stick is down
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
                if(PPM_in[ParamSet.ChannelAssignment[CH_THRUST]] < -85)
                {
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// and yaw stick is rightmost --> start motors
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
                        if(PPM_in[ParamSet.ChannelAssignment[CH_YAW]] < -75)
                        {
                                if(++delay_startmotors > 200) // not immediately (wait 200 loops = 200 * 2ms = 0.4 s)
                                {
                                        delay_startmotors = 200; // do not repeat if once executed
                                        Model_Is_Flying = 1;
                                        MotorsOn = 1;
                                        SetPointYaw = 0;
                                        Reading_IntegralGyroYaw = 0;
                                        Reading_IntegralGyroPitch = 0;
                                        Reading_IntegralGyroRoll = 0;
                                        Reading_IntegralGyroPitch2 = IntegralPitch;
                                        Reading_IntegralGyroRoll2 = IntegralRoll;
                                        SumPitch = 0;
                                        SumRoll = 0;
                                        if(ParamSet.GlobalConfig & CFG_GPS_ACTIVE)
                                        {
                                                GPS_SetHomePosition();
                                        }
                                }
                        }
                        else delay_startmotors = 0; // reset delay timer if sticks are not in this position
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// and yaw stick is leftmost --> stop motors
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
                        if(PPM_in[ParamSet.ChannelAssignment[CH_YAW]] > 75)
                                {
                                if(++delay_stopmotors > 200)  // not immediately (wait 200 loops = 200 * 2ms = 0.4 s)
                                {
                                        delay_stopmotors = 200; // do not repeat if once executed
                                        Model_Is_Flying = 0;
                                        MotorsOn = 0;
                                        if(ParamSet.GlobalConfig & CFG_GPS_ACTIVE)
                                        {
                                                GPS_ClearHomePosition();
                                        }
                                }
                        }
                        else delay_stopmotors = 0; // reset delay timer if sticks are not in this position
                }
                        // remapping of paameters only if the signal rc-sigbnal conditions are good
        } // eof RC_Quality > 150
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// new values from RC
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        if(!NewPpmData-- || EmergencyLanding) // NewData = 0 means new data from RC
        {
                int tmp_int;
                ParameterMapping(); // remapping params (online poti replacement)
                // calculate Stick inputs by rc channels (P) and changing of rc channels (D)
                StickPitch = (StickPitch * 3 + PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] * ParamSet.Stick_P) / 4;
                StickPitch += PPM_diff[ParamSet.ChannelAssignment[CH_PITCH]] * ParamSet.Stick_D;
                StickRoll = (StickRoll * 3 + PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] * ParamSet.Stick_P) / 4;
                StickRoll += PPM_diff[ParamSet.ChannelAssignment[CH_ROLL]] * ParamSet.Stick_D;
 
                // direct mapping of yaw and thrust
                StickYaw = -PPM_in[ParamSet.ChannelAssignment[CH_YAW]];
                StickThrust  = PPM_in[ParamSet.ChannelAssignment[CH_THRUST]] + 120;// shift to positive numbers
 
                // update max stick positions for pitch and roll
                if(abs(PPM_in[ParamSet.ChannelAssignment[CH_PITCH]]) > MaxStickPitch)
                        MaxStickPitch = abs(PPM_in[ParamSet.ChannelAssignment[CH_PITCH]]);
                else MaxStickPitch--;
                if(abs(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]]) > MaxStickRoll)
                        MaxStickRoll = abs(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]]);
                else MaxStickRoll--;
 
                // update gyro control loop factors
 
                Gyro_P_Factor = ((float) FCParam.Gyro_P + 10.0) / 256.0;
                Gyro_I_Factor = ((float) FCParam.Gyro_I) / 44000;
 
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// Digital Control via DubWise
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
 
                #define KEY_VALUE (FCParam.UserParam1 * 4) // step width
                if(DubWiseKeys[1]) BeepTime = 10;
                if(DubWiseKeys[1] & DUB_KEY_UP)  tmp_int = KEY_VALUE;
                else if(DubWiseKeys[1] & DUB_KEY_DOWN)  tmp_int = -KEY_VALUE;
                else tmp_int = 0;
                ExternStickPitch = (ExternStickPitch * 7 + tmp_int) / 8;
                if(DubWiseKeys[1] & DUB_KEY_LEFT)  tmp_int = KEY_VALUE;
                else if(DubWiseKeys[1] & DUB_KEY_RIGHT) tmp_int = -KEY_VALUE;
                else tmp_int = 0;
                ExternStickRoll = (ExternStickRoll * 7 + tmp_int) / 8;
 
                if(DubWiseKeys[0] & 8)  ExternStickYaw = 50;else
                if(DubWiseKeys[0] & 4)  ExternStickYaw =-50;else ExternStickYaw = 0;
                if(DubWiseKeys[0] & 2)  ExternHeightValue++;
                if(DubWiseKeys[0] & 16) ExternHeightValue--;
 
                StickPitch += ExternStickPitch / 8;
                StickRoll += ExternStickRoll / 8;
                StickYaw += ExternStickYaw;
 
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
//+ Analog control via serial communication
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
 
                if(ExternControl.Config & 0x01 && FCParam.UserParam1 > 128)
                {
                         StickPitch += (int16_t) ExternControl.Pitch * (int16_t) ParamSet.Stick_P;
                         StickRoll += (int16_t) ExternControl.Roll * (int16_t) ParamSet.Stick_P;
                         StickYaw += ExternControl.Yaw;
                         ExternHeightValue =  (int16_t) ExternControl.Height * (int16_t)ParamSet.Height_Gain;
                         if(ExternControl.Thrust < StickThrust) StickThrust = ExternControl.Thrust;
                }
                // disable I part of gyro control feedback
                if(ParamSet.GlobalConfig & CFG_HEADING_HOLD) Gyro_I_Factor =  0;
                // avoid negative scaling factors
                if(Gyro_P_Factor < 0) Gyro_P_Factor = 0;
                if(Gyro_I_Factor < 0) Gyro_I_Factor = 0;
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// Looping?
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
 
                if((PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] > ParamSet.LoopThreshold) && ParamSet.LoopConfig & CFG_LOOP_LEFT)  Looping_Left = 1;
                else
                {
                        if(Looping_Left) // Hysteresis
                        {
                                if((PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] < (ParamSet.LoopThreshold - ParamSet.LoopHysteresis))) Looping_Left = 0;
                        }
                }
                if((PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] < -ParamSet.LoopThreshold) && ParamSet.LoopConfig & CFG_LOOP_RIGHT) Looping_Right = 1;
                else
                {
                        if(Looping_Right) // Hysteresis
                        {
                                if(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]] > -(ParamSet.LoopThreshold - ParamSet.LoopHysteresis)) Looping_Right = 0;
                        }
                }
 
                if((PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] > ParamSet.LoopThreshold) && ParamSet.LoopConfig & CFG_LOOP_UP) Looping_Top = 1;
                else
                {
                        if(Looping_Top)  // Hysteresis
                        {
                                if((PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] < (ParamSet.LoopThreshold - ParamSet.LoopHysteresis))) Looping_Top = 0;
                        }
                }
                if((PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] < -ParamSet.LoopThreshold) && ParamSet.LoopConfig & CFG_LOOP_DOWN) Looping_Down = 1;
                else
                {
                        if(Looping_Down) // Hysteresis
                        {
                                if(PPM_in[ParamSet.ChannelAssignment[CH_PITCH]] > -(ParamSet.LoopThreshold - ParamSet.LoopHysteresis)) Looping_Down = 0;
                        }
                }
 
                if(Looping_Left || Looping_Right)   Looping_Roll = 1; else Looping_Roll = 0;
                if(Looping_Top  || Looping_Down) {Looping_Pitch = 1; Looping_Roll = 0; Looping_Left = 0; Looping_Right = 0;} else Looping_Pitch = 0;
        } // End of new RC-Values or Emergency Landing
 
 
        if(Looping_Roll) BeepTime = 100;
        if(Looping_Roll || Looping_Pitch)
        {
                if(ThrustMixFraction > ParamSet.LoopThrustLimit) ThrustMixFraction = ParamSet.LoopThrustLimit;
        }
 
 
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
//+ LED Control on J16/J17
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        LED1_Time = FCParam.UserParam7;
        LED2_Time = FCParam.UserParam8;
        LED_Update();
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// in case of emergency landing
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        // set all inputs to save values
        if(EmergencyLanding)
        {
                StickYaw = 0;
                StickPitch = 0;
                StickRoll = 0;
                Gyro_P_Factor  = 0.5;
                Gyro_I_Factor = 0.003;
                Looping_Roll = 0;
                Looping_Pitch = 0;
                MaxStickPitch = 0;
                MaxStickRoll = 0;
        }
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// Trim Gyro-Integrals to ACC-Signals
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
 
        #define BALANCE_NUMBER 256L
        // sum for averaging
        MeanIntegralPitch  += IntegralPitch;
        MeanIntegralRoll  += IntegralRoll;
 
        if(Looping_Pitch || Looping_Roll) // if looping in any direction
        {
                // reset averaging for acc and gyro integral as well as gyro integral acc correction
                MeasurementCounter = 0;
 
                IntegralAccPitch = 0;
                IntegralAccRoll = 0;
 
                MeanIntegralPitch = 0;
                MeanIntegralRoll = 0;
 
                Reading_IntegralGyroPitch2 = Reading_IntegralGyroPitch;
                Reading_IntegralGyroRoll2 = Reading_IntegralGyroRoll;
 
                AttitudeCorrectionPitch = 0;
                AttitudeCorrectionRoll = 0;
        }
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        if(!Looping_Pitch && !Looping_Roll) // if not lopping in any direction
        {
                int32_t tmp_long, tmp_long2;
                // determine the deviation of gyro integral from averaged acceleration sensor
                tmp_long   =  (int32_t)(IntegralPitch / ParamSet.GyroAccFactor - (int32_t)Mean_AccPitch);
                tmp_long  /= 16;
                tmp_long2  = (int32_t)(IntegralRoll   / ParamSet.GyroAccFactor - (int32_t)Mean_AccRoll);
                tmp_long2 /= 16;
 
                if((MaxStickPitch > 15) || (MaxStickRoll > 15)) // reduce effect during stick commands
                {
                        tmp_long  /= 3;
                        tmp_long2 /= 3;
                }
                if(abs(PPM_in[ParamSet.ChannelAssignment[CH_YAW]]) > 25) // reduce further if yaw stick is active
                {
                        tmp_long  /= 3;
                        tmp_long2 /= 3;
                }
 
                #define BALANCE 32
                // limit correction effect
                if(tmp_long >  BALANCE)  tmp_long  = BALANCE;
                if(tmp_long < -BALANCE)  tmp_long  =-BALANCE;
                if(tmp_long2 > BALANCE)  tmp_long2 = BALANCE;
                if(tmp_long2 <-BALANCE)  tmp_long2 =-BALANCE;
                // correct current readings
                Reading_IntegralGyroPitch -= tmp_long;
                Reading_IntegralGyroRoll -= tmp_long2;
        }
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        // MeasurementCounter is incremented in the isr of analog.c
        if(MeasurementCounter >= BALANCE_NUMBER) // averaging number has reached
        {
                static int16_t cnt = 0;
                static int8_t last_n_p, last_n_n, last_r_p, last_r_n;
                static int32_t MeanIntegralPitch_old, MeanIntegralRoll_old;
 
                // if not lopping in any direction (this should be alwais the case,
                // because the Measurement counter is reset to 0 if looping in any direction is active.)
                if(!Looping_Pitch && !Looping_Roll)
                {
                        // Calculate mean value of the gyro integrals
                        MeanIntegralPitch /= BALANCE_NUMBER;
                        MeanIntegralRoll  /= BALANCE_NUMBER;
 
                        // Calculate mean of the acceleration values
                        IntegralAccPitch = (ParamSet.GyroAccFactor * IntegralAccPitch) / BALANCE_NUMBER;
                        IntegralAccRoll  = (ParamSet.GyroAccFactor * IntegralAccRoll ) / BALANCE_NUMBER;
 
                        // Pitch ++++++++++++++++++++++++++++++++++++++++++++++++
                        // Calculate deviation of the averaged gyro integral and the averaged acceleration integral
                        IntegralErrorPitch = (int32_t)(MeanIntegralPitch - (int32_t)IntegralAccPitch);
                        CorrectionPitch = IntegralErrorPitch / ParamSet.GyroAccTrim;
                        AttitudeCorrectionPitch = CorrectionPitch / BALANCE_NUMBER;
                        // Roll ++++++++++++++++++++++++++++++++++++++++++++++++
                        // Calculate deviation of the averaged gyro integral and the averaged acceleration integral
                        IntegralErrorRoll = (int32_t)(MeanIntegralRoll - (int32_t)IntegralAccRoll);
                        CorrectionRoll  = IntegralErrorRoll / ParamSet.GyroAccTrim;
                        AttitudeCorrectionRoll  = CorrectionRoll  / BALANCE_NUMBER;
 
                        if((MaxStickPitch > 15) || (MaxStickRoll > 15) || (abs(PPM_in[ParamSet.ChannelAssignment[CH_YAW]]) > 25))
                        {
                                AttitudeCorrectionPitch /= 2;
                                AttitudeCorrectionRoll /= 2;
                        }
 
        // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        // Gyro-Drift ermitteln
        // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
                        // deviation of gyro pitch integral (IntegralPitch is corrected by averaged acc sensor)
                        IntegralErrorPitch  = IntegralPitch2 - IntegralPitch;
                        Reading_IntegralGyroPitch2 -= IntegralErrorPitch;
                        // deviation of gyro pitch integral (IntegralPitch is corrected by averaged acc sensor)
                        IntegralErrorRoll = IntegralRoll2 - IntegralRoll;
                        Reading_IntegralGyroRoll2 -= IntegralErrorRoll;
 
 
                        // DebugOut.Analog[17] = IntegralAccPitch / 26;
                        DebugOut.Analog[18] = IntegralAccRoll / 26;
                        DebugOut.Analog[19] = IntegralErrorPitch;// / 26;
                        DebugOut.Analog[20] = IntegralErrorRoll;// / 26;
                        DebugOut.Analog[21] = MeanIntegralPitch / 26;
                        DebugOut.Analog[22] = MeanIntegralRoll / 26;
                        //DebugOut.Analog[28] = CorrectionPitch;
                        DebugOut.Analog[29] = CorrectionRoll;
                        DebugOut.Analog[30] = AttitudeCorrectionRoll * 10;
 
                        #define ERROR_LIMIT  (BALANCE_NUMBER * 4)
                        #define ERROR_LIMIT2 (BALANCE_NUMBER * 16)
                        #define MOVEMENT_LIMIT 20000
        // Pitch +++++++++++++++++++++++++++++++++++++++++++++++++
                        cnt = 1;// + labs(IntegralErrorPitch) / 4096;
                        CorrectionPitch = 0;
                        if(labs(MeanIntegralPitch_old - MeanIntegralPitch) < MOVEMENT_LIMIT)
                        {
                                if(IntegralErrorPitch >  ERROR_LIMIT2)
                                {
                                        if(last_n_p)
                                        {
                                                cnt += labs(IntegralErrorPitch) / ERROR_LIMIT2;
                                                CorrectionPitch = IntegralErrorPitch / 8;
                                                if(CorrectionPitch > 5000) CorrectionPitch = 5000;
                                                AttitudeCorrectionPitch += CorrectionPitch / BALANCE_NUMBER;
                                        }
                                        else last_n_p = 1;
                                }
                                else  last_n_p = 0;
                                if(IntegralErrorPitch < -ERROR_LIMIT2)
                                {
                                        if(last_n_n)
                                        {
                                                cnt += labs(IntegralErrorPitch) / ERROR_LIMIT2;
                                                CorrectionPitch = IntegralErrorPitch / 8;
                                                if(CorrectionPitch < -5000) CorrectionPitch = -5000;
                                                AttitudeCorrectionPitch += CorrectionPitch / BALANCE_NUMBER;
                                        }
                                        else last_n_n = 1;
                                }
                                else  last_n_n = 0;
                        }
                        else cnt = 0;
                        if(cnt > ParamSet.DriftComp) cnt = ParamSet.DriftComp;
                        // correct Gyro Offsets
                        if(IntegralErrorPitch >  ERROR_LIMIT)   AdNeutralPitch += cnt;
                        if(IntegralErrorPitch < -ERROR_LIMIT)   AdNeutralPitch -= cnt;
 
        // Roll +++++++++++++++++++++++++++++++++++++++++++++++++
                        cnt = 1;// + labs(IntegralErrorPitch) / 4096;
                        CorrectionRoll = 0;
                        if(labs(MeanIntegralRoll_old - MeanIntegralRoll) < MOVEMENT_LIMIT)
                        {
                                if(IntegralErrorRoll >  ERROR_LIMIT2)
                                {
                                        if(last_r_p)
                                        {
                                                cnt += labs(IntegralErrorRoll) / ERROR_LIMIT2;
                                                CorrectionRoll = IntegralErrorRoll / 8;
                                                if(CorrectionRoll > 5000) CorrectionRoll = 5000;
                                                AttitudeCorrectionRoll += CorrectionRoll / BALANCE_NUMBER;
                                        }
                                        else last_r_p = 1;
                                }
                                else  last_r_p = 0;
                                if(IntegralErrorRoll < -ERROR_LIMIT2)
                                {
                                        if(last_r_n)
                                        {
                                                cnt += labs(IntegralErrorRoll) / ERROR_LIMIT2;
                                                CorrectionRoll = IntegralErrorRoll / 8;
                                                if(CorrectionRoll < -5000) CorrectionRoll = -5000;
                                                AttitudeCorrectionRoll += CorrectionRoll / BALANCE_NUMBER;
                                        }
                                        else last_r_n = 1;
                                }
                                else  last_r_n = 0;
                        }
                        else cnt = 0;
                        // correct Gyro Offsets
                        if(cnt > ParamSet.DriftComp) cnt = ParamSet.DriftComp;
                        if(IntegralErrorRoll >  ERROR_LIMIT)   AdNeutralRoll += cnt;
                        if(IntegralErrorRoll < -ERROR_LIMIT)   AdNeutralRoll -= cnt;
 
                        DebugOut.Analog[27] = CorrectionRoll;
                        DebugOut.Analog[23] = AdNeutralPitch;//10*(AdNeutralPitch - StartNeutralPitch);
                        DebugOut.Analog[24] = 10*(AdNeutralRoll - StartNeutralRoll);
                }
                else // looping is active
                {
                        AttitudeCorrectionRoll  = 0;
                        AttitudeCorrectionPitch = 0;
                }
 
                // if Gyro_I_Factor == 0 , for example at Heading Hold, ignore attitude correction
                if(!Gyro_I_Factor)
                {
                        AttitudeCorrectionRoll  = 0;
                        AttitudeCorrectionPitch = 0;
                }
        // +++++++++++++++++++++++++++++++++++++++++++++++++++++
                MeanIntegralPitch_old = MeanIntegralPitch;
                MeanIntegralRoll_old  = MeanIntegralRoll;
        // +++++++++++++++++++++++++++++++++++++++++++++++++++++
                // reset variables used for averaging
                IntegralAccPitch = 0;
                IntegralAccRoll = 0;
                MeanIntegralPitch = 0;
                MeanIntegralRoll = 0;
                MeasurementCounter = 0;
        } // end of averaging
 
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
//  Yawing
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        if(abs(StickYaw) > 20 ) // yaw stick is activated
        {
                if(!(ParamSet.GlobalConfig & CFG_COMPASS_FIX)) UpdateCompassCourse = 1;
        }
        // exponential stick sensitivity in yawring rate
        tmp_int  = (int32_t) ParamSet.Yaw_P * ((int32_t)StickYaw * abs(StickYaw)) / 512L; // expo  y = ax + bx²
        tmp_int += (ParamSet.Yaw_P * StickYaw) / 4;
        SetPointYaw = tmp_int;
        // trimm drift of Reading_IntegralGyroYaw with SetPointYaw(StickYaw)
        Reading_IntegralGyroYaw -= tmp_int;
        // limit the effect
        if(Reading_IntegralGyroYaw > 50000) Reading_IntegralGyroYaw = 50000;
        if(Reading_IntegralGyroYaw <-50000) Reading_IntegralGyroYaw =-50000;
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
//  Compass
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
    // compass code is used if Compass option or GPS option is selected
        if((ParamSet.GlobalConfig & CFG_COMPASS_ACTIVE) || (ParamSet.GlobalConfig & CFG_GPS_ACTIVE))
        {
                static uint8_t updCompass = 0;
                int16_t w,v;
 
                if (!updCompass--)
                {
                        updCompass = 49; // update only at 2ms*50 = 100ms (10Hz)
                        // get current compass heading (angle between MK head and magnetic north)
                        #ifdef USE_MM3
                        CompassHeading = MM3_Heading();
                        #endif
                        #ifdef USE_CMPS03
                        CompassHeading = CMPS03_Heading();
                        #endif
                        if (CompassHeading < 0) CompassOffCourse = 0; // disable gyro compass correction on bad compass data
                        else CompassOffCourse = ((540 + CompassHeading - CompassCourse) % 360) - 180; // calc course deviation
                }
 
                // get maximum attitude angle
                w = abs(IntegralPitch/512);
                v = abs(IntegralRoll /512);
                if(v > w) w = v;
                if (w < 25)
                {
                        if(UpdateCompassCourse)
                        {
                                UpdateCompassCourse = 0;
                                CompassCourse = CompassHeading;
                                CompassOffCourse = 0;
                        }
                        w = (w * FCParam.CompassYawEffect) / 64;
                w = FCParam.CompassYawEffect - w;
                        if(w > 0) Reading_IntegralGyroYaw += (CompassOffCourse * w) / 32;
                }
        }
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
//  GPS
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        if(ParamSet.GlobalConfig & CFG_GPS_ACTIVE)
        {
                GPS_I_Factor = FCParam.UserParam2;
                GPS_P_Factor = FCParam.UserParam5;
                GPS_D_Factor = FCParam.UserParam6;
                if(EmergencyLanding) GPS_Main(230); // enables Comming Home
                else GPS_Main(Poti3);               // behavior controlled by Poti3
        }
        else
        {
                GPS_Neutral();
        }
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
//  Debugwerte zuordnen
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        if(!TimerDebugOut--)
        {
                TimerDebugOut = 24; // update debug outputs every 25*2ms = 50 ms (20Hz)
                DebugOut.Analog[0]  = IntegralPitch / ParamSet.GyroAccFactor;
                DebugOut.Analog[1]  = IntegralRoll / ParamSet.GyroAccFactor;
                DebugOut.Analog[2]  = Mean_AccPitch;
                DebugOut.Analog[3]  = Mean_AccRoll;
                DebugOut.Analog[4]  = Reading_GyroYaw;
                DebugOut.Analog[5]  = ReadingHeight;
                DebugOut.Analog[6]  = (Reading_Integral_Top / 512);
                DebugOut.Analog[8]  = CompassHeading;
                DebugOut.Analog[9]  = UBat;
                DebugOut.Analog[10] = RC_Quality;
                //DebugOut.Analog[11] = RC_Quality;
                //DebugOut.Analog[16] = Mean_AccTop;
 
                /*    DebugOut.Analog[16] = motor_rx[0];
                DebugOut.Analog[17] = motor_rx[1];
                DebugOut.Analog[18] = motor_rx[2];
                DebugOut.Analog[19] = motor_rx[3];
                DebugOut.Analog[20] = motor_rx[0] + motor_rx[1] + motor_rx[2] + motor_rx[3];
                DebugOut.Analog[20] /= 14;
                DebugOut.Analog[21] = motor_rx[4];
                DebugOut.Analog[22] = motor_rx[5];
                DebugOut.Analog[23] = motor_rx[6];
                DebugOut.Analog[24] = motor_rx[7];
                DebugOut.Analog[25] = motor_rx[4] + motor_rx[5] + motor_rx[6] + motor_rx[7];
 
                DebugOut.Analog[9]  = Reading_GyroPitch;
                DebugOut.Analog[9]  = SetPointHeight;
                DebugOut.Analog[10] = Reading_IntegralGyroYaw / 128;
 
                DebugOut.Analog[10] = FCParam.Gyro_I;
                DebugOut.Analog[10] = ParamSet.Gyro_I;
                DebugOut.Analog[9]  = CompassOffCourse;
                DebugOut.Analog[10] = ThrustMixFraction;
                DebugOut.Analog[3]  = HeightD * 32;
                DebugOut.Analog[4]  = HeightControlThrust;
                */
        }
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
//  calculate control feedback from angle (gyro integral) and agular velocity (gyro signal)
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
 
        if(Looping_Pitch) Reading_GyroPitch = Reading_GyroPitch * Gyro_P_Factor;
        else Reading_GyroPitch = IntegralPitch * Gyro_I_Factor + Reading_GyroPitch * Gyro_P_Factor;
        if(Looping_Roll) Reading_GyroRoll = Reading_GyroRoll * Gyro_P_Factor;
        else Reading_GyroRoll = IntegralRoll * Gyro_I_Factor + Reading_GyroRoll * Gyro_P_Factor;
        Reading_GyroYaw = Reading_GyroYaw * (2 * Gyro_P_Factor) + IntegralYaw * Gyro_I_Factor / 2;
 
        DebugOut.Analog[25] = IntegralRoll * Gyro_I_Factor;
        DebugOut.Analog[31] = StickRoll;// / (26*Gyro_I_Factor);
        DebugOut.Analog[28] = Reading_GyroRoll;
 
        // limit control feedback
        #define MAX_SENSOR  2048
        if(Reading_GyroPitch >  MAX_SENSOR) Reading_GyroPitch =  MAX_SENSOR;
        if(Reading_GyroPitch < -MAX_SENSOR) Reading_GyroPitch = -MAX_SENSOR;
        if(Reading_GyroRoll  >  MAX_SENSOR) Reading_GyroRoll  =  MAX_SENSOR;
        if(Reading_GyroRoll  < -MAX_SENSOR) Reading_GyroRoll  = -MAX_SENSOR;
        if(Reading_GyroYaw   >  MAX_SENSOR) Reading_GyroYaw   =  MAX_SENSOR;
        if(Reading_GyroYaw   < -MAX_SENSOR) Reading_GyroYaw   = -MAX_SENSOR;
 
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// Height Control
// The height control algorithm reduces the thrust but does not increase the thrust.
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        // If height control is activated and no emergency landing is active
        if((ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL) && (!EmergencyLanding) )
        {
                int tmp_int;
                // if height control is activated by an rc channel
                if(ParamSet.GlobalConfig & CFG_HEIGHT_SWITCH)
                {       // check if parameter is less than activation threshold
                        if(FCParam.MaxHeight < 50)
                        {
                                SetPointHeight = ReadingHeight - 20;  // update SetPoint with current reading
                                HeightControlActive = 0; // disable height control
                        }
                        else HeightControlActive = 1; // enable height control
                }
                else // no switchable height control
                {
                        SetPointHeight = ((int16_t) ExternHeightValue + (int16_t) FCParam.MaxHeight) * (int16_t)ParamSet.Height_Gain - 20;
                        HeightControlActive = 1;
                }
                // get current height
                h = ReadingHeight;
                // if current height is above the setpoint reduce thrust
                if((h > SetPointHeight) && HeightControlActive)
                {
                        // ThrustMixFraction - HightDeviation * P  - HeightChange * D - ACCTop * DACC
                        // height difference -> P control part
                        h = ((h - SetPointHeight) * (int16_t) FCParam.Height_P) / 16;
                        h = ThrustMixFraction - h; // reduce gas
                        // height gradient --> D control part
                        h -= (HeightD * FCParam.Height_D) / 8;  // D control part
                        // acceleration sensor effect
                        tmp_int = ((Reading_Integral_Top / 512) * (int32_t) FCParam.Height_ACC_Effect) / 32;
                        if(tmp_int > 50) tmp_int = 50;
                        if(tmp_int < -50) tmp_int = -50;
                        h -= tmp_int;
                        // update height control thrust
                        HeightControlThrust = (HeightControlThrust*15 + h) / 16;
                        // limit thrust reduction
                        if(HeightControlThrust < ParamSet.Height_MinThrust)
                        {
                                if(ThrustMixFraction >= ParamSet.Height_MinThrust) HeightControlThrust = ParamSet.Height_MinThrust;
                                // allows landing also if thrust stick is reduced below min thrust on height control
                                if(ThrustMixFraction < ParamSet.Height_MinThrust) HeightControlThrust = ThrustMixFraction;
                        }
                        // limit thrust to stick setting
                        if(HeightControlThrust > ThrustMixFraction) HeightControlThrust = ThrustMixFraction;
                        ThrustMixFraction = HeightControlThrust;
                }
        }
        // limit thrust to parameter setting
        if(ThrustMixFraction > ParamSet.Trust_Max - 20) ThrustMixFraction = ParamSet.Trust_Max - 20;
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + Mixer and PI-Controller
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
 
        DebugOut.Analog[7] = ThrustMixFraction;
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// Yaw-Fraction
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
    YawMixFraction = Reading_GyroYaw - SetPointYaw;     // yaw controller
 
        // limit YawMixFraction
    if(YawMixFraction > (ThrustMixFraction / 2)) YawMixFraction = ThrustMixFraction / 2;
    if(YawMixFraction < -(ThrustMixFraction / 2)) YawMixFraction = -(ThrustMixFraction / 2);
    if(YawMixFraction > ((ParamSet.Trust_Max - ThrustMixFraction))) YawMixFraction = ((ParamSet.Trust_Max - ThrustMixFraction));
    if(YawMixFraction < -((ParamSet.Trust_Max - ThrustMixFraction))) YawMixFraction = -((ParamSet.Trust_Max - ThrustMixFraction));
    if(ThrustMixFraction < 20) YawMixFraction = 0;
       
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// Pitch-Axis
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
    DiffPitch = Reading_GyroPitch - (StickPitch - GPS_Pitch);   // get difference
    if(Gyro_I_Factor) SumPitch += IntegralPitch * Gyro_I_Factor - (StickPitch - GPS_Pitch); // I-part for attitude control
    else SumPitch += DiffPitch; // I-part for head holding
    if(SumPitch >  16000) SumPitch =  16000;
    if(SumPitch < -16000) SumPitch = -16000;
    pd_result = DiffPitch + Ki * SumPitch; // PI-controller for pitch
 
    tmp_int = (int32_t)((int32_t)FCParam.DynamicStability * (int32_t)(ThrustMixFraction + abs(YawMixFraction)/2)) / 64;
    if(pd_result >  tmp_int) pd_result =  tmp_int;
    if(pd_result < -tmp_int) pd_result = -tmp_int;
       
        PitchMixFraction = pd_result;  
       
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// Roll-Axis
// +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
        DiffRoll = Reading_GyroRoll - (StickRoll  - GPS_Roll);  // get difference
    if(Gyro_I_Factor) SumRoll += IntegralRoll * Gyro_I_Factor - (StickRoll  - GPS_Roll); // I-part for attitude control
    else SumRoll += DiffRoll;  // I-part for head holding
    if(SumRoll >  16000) SumRoll =  16000;
    if(SumRoll < -16000) SumRoll = -16000;
    pd_result = DiffRoll + Ki * SumRoll;         // PI-controller for roll
    tmp_int = (int32_t)((int32_t)FCParam.DynamicStability * (int32_t)(ThrustMixFraction + abs(YawMixFraction)/2)) / 64;
    if(pd_result >  tmp_int) pd_result =  tmp_int;
    if(pd_result < -tmp_int) pd_result = -tmp_int;
 
    RollMixFraction = pd_result;
 
// Calculate Motor Mixes
       
        // Motor FrontLeft
    MotorValue =        ThrustMixFraction
                                        + PitchMixFraction
                                        + RollMixFraction/2
                                        - YawMixFraction;         // Mixer
        if ((MotorValue < 0)) MotorValue = 0;
        else if(MotorValue > ParamSet.Trust_Max)            MotorValue = ParamSet.Trust_Max;
        if (MotorValue < ParamSet.Trust_Min)            MotorValue = ParamSet.Trust_Min;
        Motor_FrontLeft = MotorValue;
 
        // Motor FrontRight
    MotorValue =        ThrustMixFraction
                                        + PitchMixFraction
                                        - RollMixFraction/2
                                        + YawMixFraction;         // Mixer
        if ((MotorValue < 0)) MotorValue = 0;
        else if(MotorValue > ParamSet.Trust_Max)            MotorValue = ParamSet.Trust_Max;
        if (MotorValue < ParamSet.Trust_Min)            MotorValue = ParamSet.Trust_Min;
        Motor_FrontRight = MotorValue;
 
        // Motor RearLeft
        MotorValue =    ThrustMixFraction
                                        - PitchMixFraction
                                        + RollMixFraction/2
                                        - YawMixFraction;     // Mixer
        if ((MotorValue < 0)) MotorValue = 0;
        else if(MotorValue > ParamSet.Trust_Max)            MotorValue = ParamSet.Trust_Max;
        if (MotorValue < ParamSet.Trust_Min)            MotorValue = ParamSet.Trust_Min;
        Motor_RearLeft = MotorValue;
        // Motor RearRight
        MotorValue =    ThrustMixFraction
                                        - PitchMixFraction
                                        - RollMixFraction/2
                                        + YawMixFraction;     // Mixer
        if ((MotorValue < 0)) MotorValue = 0;
        else if(MotorValue > ParamSet.Trust_Max)            MotorValue = ParamSet.Trust_Max;
        if (MotorValue < ParamSet.Trust_Min)            MotorValue = ParamSet.Trust_Min;
        Motor_RearRight= MotorValue;
       
    // Motor Left
    MotorValue =        ThrustMixFraction
                                        + RollMixFraction
                                        + YawMixFraction;  // Mixer
        if ((MotorValue < 0)) MotorValue = 0;
        else if(MotorValue > ParamSet.Trust_Max)                MotorValue = ParamSet.Trust_Max;
        if (MotorValue < ParamSet.Trust_Min)            MotorValue = ParamSet.Trust_Min;
    Motor_Left = MotorValue;
 
        // Motor Right
        MotorValue =    ThrustMixFraction
                                        - RollMixFraction
                                        - YawMixFraction;  // Mixer
        if ((MotorValue < 0)) MotorValue = 0;
        else if(MotorValue > ParamSet.Trust_Max)                MotorValue = ParamSet.Trust_Max;
        if (MotorValue < ParamSet.Trust_Min)            MotorValue = ParamSet.Trust_Min;
    Motor_Right = MotorValue;
}
 
 
Subversion Repositories FlightCtrl

(root)/branches/V0.68d CRK HexaLotte/fc.c - Rev 898 → 2147
