Rev 2110 | Rev 2130 | Go to most recent revision | Details | Compare with Previous | Last modification | View Log | RSS feed
Rev | Author | Line No. | Line |
---|---|---|---|
2108 | - | 1 | #include <avr/boot.h> |
2 | #include <avr/io.h> |
||
3 | #include <avr/interrupt.h> |
||
4 | #include <util/delay.h> |
||
5 | |||
6 | #include "timer0.h" |
||
7 | #include "timer2.h" |
||
8 | #include "uart0.h" |
||
9 | #include "output.h" |
||
10 | #include "attitude.h" |
||
11 | #include "commands.h" |
||
12 | #include "flight.h" |
||
13 | #include "rc.h" |
||
14 | #include "analog.h" |
||
15 | #include "configuration.h" |
||
16 | #include "controlMixer.h" |
||
17 | #include "eeprom.h" |
||
18 | #include "printf_P.h" |
||
19 | |||
20 | int16_t main(void) { |
||
21 | uint16_t timer; |
||
22 | |||
23 | // disable interrupts global |
||
24 | cli(); |
||
25 | |||
26 | // disable watchdog |
||
27 | MCUSR &= ~(1 << WDRF); |
||
28 | WDTCSR |= (1 << WDCE) | (1 << WDE); |
||
29 | WDTCSR = 0; |
||
30 | |||
31 | // This is strange: It should NOT be necessarty to do. But the call of the same, |
||
32 | // in channelMap_readOrDefault (if eeprom read fails) just sets all to 0,0,0,.... |
||
2109 | - | 33 | channelMap_default(); |
2108 | - | 34 | |
35 | // initalize modules |
||
36 | output_init(); |
||
37 | timer0_init(); |
||
38 | timer2_init(); |
||
39 | usart0_init(); |
||
40 | RC_Init(); |
||
41 | analog_init(); |
||
42 | |||
43 | // Parameter Set handling |
||
44 | IMUConfig_readOrDefault(); |
||
45 | channelMap_readOrDefault(); |
||
46 | paramSet_readOrDefault(); |
||
47 | |||
48 | // enable interrupts global |
||
49 | sei(); |
||
50 | |||
51 | printf("\n\r==================================="); |
||
52 | printf("\n\rFlightControl"); |
||
53 | printf("\n\rHardware: Custom"); |
||
54 | printf("\n\r CPU: Atmega328"); |
||
2109 | - | 55 | printf("\n\rSoftware: V%d.%d%c", |
56 | VERSION_MAJOR, VERSION_MINOR, VERSION_PATCH + 'a'); |
||
2108 | - | 57 | printf("\n\r==================================="); |
58 | |||
59 | // Wait for a short time (otherwise the RC channel check won't work below) |
||
60 | // timer = SetDelay(500); |
||
61 | // while(!CheckDelay(timer)); |
||
62 | |||
63 | // Instead, while away the time by flashing the 2 outputs: |
||
64 | // First J16, then J17. Makes it easier to see which is which. |
||
65 | timer = setDelay(200); |
||
2109 | - | 66 | outputSet(0, 1); |
2108 | - | 67 | GRN_OFF; |
68 | RED_ON; |
||
69 | while (!checkDelay(timer)) |
||
70 | ; |
||
71 | |||
72 | timer = setDelay(200); |
||
2109 | - | 73 | outputSet(0, 0); |
74 | outputSet(1, 1); |
||
2108 | - | 75 | RED_OFF; |
76 | GRN_ON; |
||
77 | while (!checkDelay(timer)) |
||
78 | ; |
||
79 | |||
80 | timer = setDelay(200); |
||
81 | while (!checkDelay(timer)) |
||
82 | ; |
||
2109 | - | 83 | outputSet(1, 0); |
2108 | - | 84 | GRN_OFF; |
85 | |||
2109 | - | 86 | printf("\n\r==================================="); |
2108 | - | 87 | |
88 | #ifdef USE_NAVICTRL |
||
89 | printf("\n\rSupport for NaviCtrl"); |
||
90 | #endif |
||
91 | |||
92 | #ifdef USE_DIRECT_GPS |
||
93 | printf("\n\rDirect (no NaviCtrl) navigation"); |
||
94 | #endif |
||
95 | |||
96 | controlMixer_setNeutral(); |
||
97 | |||
98 | // Cal. attitude sensors and reset integrals. |
||
99 | attitude_setNeutral(); |
||
100 | |||
101 | // Init flight parameters |
||
102 | // flight_setNeutral(); |
||
103 | |||
104 | beep(2000); |
||
105 | |||
106 | printf("\n\n\r"); |
||
107 | |||
2109 | - | 108 | while (1) { |
2108 | - | 109 | if (runFlightControl) { // control interval |
110 | runFlightControl = 0; // reset Flag, is enabled every 2 ms by ISR of timer0 |
||
111 | if (sensorDataReady != ALL_DATA_READY) { |
||
112 | // Analog data should have been ready but is not!! |
||
113 | debugOut.digital[0] |= DEBUG_MAINLOOP_TIMER; |
||
114 | } else { |
||
115 | debugOut.digital[0] &= ~DEBUG_MAINLOOP_TIMER; |
||
2109 | - | 116 | } |
2110 | - | 117 | PD2HIGH; |
2109 | - | 118 | // This is probably the correct order: |
119 | // The attitude computation should not depend on anything from control (except maybe the estimation of control activity level) |
||
120 | // The control may depend on attitude - for example, attitude control uses pitch and roll angles, compass control uses yaw angle etc. |
||
121 | // Flight control uses results from both. |
||
122 | calculateFlightAttitude(); |
||
123 | controlMixer_periodicTask(); |
||
124 | commands_handleCommands(); |
||
125 | flight_control(); |
||
2110 | - | 126 | PD2LOW; |
2108 | - | 127 | |
2109 | - | 128 | // Allow Serial Data Transmit if motors must not updated or motors are not running |
129 | if (!runFlightControl || !isFlying) { |
||
130 | usart0_transmitTxData(); |
||
131 | } |
||
2108 | - | 132 | |
2109 | - | 133 | usart0_processRxData(); |
2108 | - | 134 | |
2109 | - | 135 | if (checkDelay(timer)) { |
136 | // Do nothing. The voltage on the input side of the regulator is <5V; |
||
137 | // we must be running off USB power. Keep it quiet. |
||
2119 | - | 138 | } else if (UBat < staticParams.batteryWarningVoltage && UBat > UBAT_AT_5V) { |
2109 | - | 139 | beepBatteryAlarm(); |
2108 | - | 140 | } |
141 | |||
2109 | - | 142 | timer = setDelay(20); // every 20 ms |
143 | output_update(); |
||
144 | } |
||
2108 | - | 145 | |
2109 | - | 146 | calculateFeaturedServoValues(); |
147 | |||
148 | if (runFlightControl) { // Time for the next iteration was up before the current finished. Signal error. |
||
149 | debugOut.digital[1] |= DEBUG_MAINLOOP_TIMER; |
||
150 | } else { |
||
151 | debugOut.digital[1] &= ~DEBUG_MAINLOOP_TIMER; |
||
2108 | - | 152 | } |
153 | } |
||
154 | return (1); |
||
155 | } |