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https://github.com/ArduPilot/ardupilot
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SITL: Add V2 telemetry protocol to IE24 fuel cell
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@ -29,13 +29,15 @@ extern const AP_HAL::HAL& hal;
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using namespace SITL;
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#define MAX_TANK_PRESSURE 300 //(bar)
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// table of user settable parameters
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const AP_Param::GroupInfo IntelligentEnergy24::var_info[] = {
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// @Param: ENABLE
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// @DisplayName: IntelligentEnergy 2.4kWh FuelCell sim enable/disable
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// @Description: Allows you to enable (1) or disable (0) the FuelCell simulator
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// @Values: 0:Disabled,1:Enabled
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// @Values: 0:Disabled,1:V1 Protocol,2:V2 Protocol
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// @User: Advanced
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AP_GROUPINFO("ENABLE", 1, IntelligentEnergy24, enabled, 0),
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@ -70,9 +72,9 @@ void IntelligentEnergy24::update(const struct sitl_input &input)
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void IntelligentEnergy24::update_send()
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{
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// just send a chunk of data at 1Hz:
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// just send a chunk of data at 2 Hz:
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const uint32_t now = AP_HAL::millis();
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if (now - last_sent_ms < 500) {
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if (now - last_data_sent_ms < 500) {
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return;
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}
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@ -80,7 +82,7 @@ void IntelligentEnergy24::update_send()
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float amps = discharge ? -20.0f : 20.0f;
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// Update pack capacity remaining
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bat_capacity_mAh += amps*(now - last_sent_ms)/3600.0f;
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bat_capacity_mAh += amps*(now - last_data_sent_ms)/3600.0f;
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// From capacity remaining approximate voltage by linear interpolation
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const float min_bat_vol = 42.0f;
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@ -90,7 +92,7 @@ void IntelligentEnergy24::update_send()
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// Simulate tank pressure
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// Scale tank pressure linearly to a percentage.
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// Min = 5 bar, max = 300 bar, PRESS_GRAD = 1/295.
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const int16_t tank_bar = linear_interpolate(5, 295, bat_capacity_mAh / max_bat_capactiy_mAh, 0, 1);
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const int16_t tank_bar = linear_interpolate(5, MAX_TANK_PRESSURE, bat_capacity_mAh / max_bat_capactiy_mAh, 0, 1);
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battery_voltage = bat_capacity_mAh / max_bat_capactiy_mAh * (max_bat_vol - min_bat_vol) + min_bat_vol;
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@ -112,10 +114,13 @@ void IntelligentEnergy24::update_send()
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state = 2; // Running
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}
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last_sent_ms = now;
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last_data_sent_ms = now;
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char message[128];
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hal.util->snprintf(message, ARRAY_SIZE(message), "<%i,%.1f,%i,%u,%i,%u,%u>\n",
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if (enabled.get() == 1) {
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// V1 Protocol
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hal.util->snprintf(message, ARRAY_SIZE(message), "<%i,%.1f,%i,%u,%i,%u,%u>\n",
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tank_bar,
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battery_voltage,
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(signed)pwr_out,
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@ -124,6 +129,54 @@ void IntelligentEnergy24::update_send()
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(unsigned)state,
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(unsigned)err_code);
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} else {
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// V2 Protocol
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// version message sent at 0.2 Hz
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if (now - last_ver_sent_ms > 5e3) {
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// PCM software part number, software version number, protocol number, hardware serial number, check-sum
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hal.util->snprintf(message, ARRAY_SIZE(message), "[10011867,2.132,4,IE12160A8040015,7]\n");
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if ((unsigned)write_to_autopilot(message, strlen(message)) != strlen(message)) {
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AP_HAL::panic("Failed to write to autopilot: %s", strerror(errno));
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}
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last_ver_sent_ms = now;
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}
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// data message
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memset(&message, 0, sizeof(message));
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int8_t tank_remaining_pct = (float)tank_bar / MAX_TANK_PRESSURE * 100.0;
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hal.util->snprintf(message, ARRAY_SIZE(message), "<%i,%.2f,%.1f,%i,%u,%i,%i,%u,%u,%i,,", // last blank , is for fuel cell to send info string up to 32 char ASCII
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tank_remaining_pct,
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0.67f, // inlet pressure (bar)
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battery_voltage,
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(signed)pwr_out,
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(unsigned)spm_pwr,
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0, // unit at fault (0 = no fault)
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(signed)battery_pwr,
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(unsigned)state,
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(unsigned)err_code,
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0); // fault state 2 (0 = no fault)
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// calculate the checksum
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uint8_t checksum = 0;
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for (uint8_t i = 0; i < ARRAY_SIZE(message); i++) {
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if (message[i] == 0) {
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break;
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}
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checksum += message[i];
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}
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// checksum is inverted 8-bit
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checksum = ~checksum;
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// add the checksum to the end of the message
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char data_end[7];
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hal.util->snprintf(data_end, ARRAY_SIZE(data_end), "%u>\n", checksum);
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strncat(message, data_end, ARRAY_SIZE(data_end));
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}
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if ((unsigned)write_to_autopilot(message, strlen(message)) != strlen(message)) {
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AP_HAL::panic("Failed to write to autopilot: %s", strerror(errno));
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}
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@ -67,7 +67,8 @@ private:
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float battery_voltage = 50.4f;
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float bat_capacity_mAh = 3300;
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bool discharge = true; // used to switch between battery charging and discharging
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uint32_t last_sent_ms;
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uint32_t last_data_sent_ms;
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uint32_t last_ver_sent_ms;
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};
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