mirror of https://github.com/ArduPilot/ardupilot
SITL: VectorNav: update simulated VN-300 for new packet type
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759f035636
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621e01fbcc
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@ -20,6 +20,7 @@
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#include <stdio.h>
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#include <unistd.h>
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#include <fcntl.h>
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#include <AP_Common/NMEA.h>
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using namespace SITL;
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@ -29,21 +30,16 @@ VectorNav::VectorNav() :
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}
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struct PACKED VN_packet1 {
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uint64_t timeStartup;
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uint64_t timeGPS;
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float uncompMag[3];
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float uncompAccel[3];
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float uncompAngRate[3];
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float pressure;
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float mag[3];
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float accel[3];
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float gyro[3];
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uint16_t sensSat;
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uint16_t AHRSStatus;
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float ypr[3];
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float quaternion[4];
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float linAccBody[3];
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float yprU[3];
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uint16_t INSStatus;
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double positionLLA[3];
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float velNED[3];
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float posU;
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@ -60,11 +56,10 @@ struct PACKED VN_packet2 {
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float GPS1DOP[7];
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uint8_t numGPS2Sats;
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uint8_t GPS2Fix;
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float GPS2DOP[7];
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};
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#define VN_PKT1_HEADER { 0xfa, 0x35, 0x03, 0x00, 0x2c, 0x0f, 0x47, 0x01, 0x13, 0x06 }
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#define VN_PKT2_HEADER { 0xfa, 0x4e, 0x02, 0x00, 0x10, 0x00, 0xb8, 0x20, 0x18, 0x20 }
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#define VN_PKT1_HEADER { 0xFA, 0x34, 0x2E, 0x07, 0x06, 0x01, 0x12, 0x06 }
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#define VN_PKT2_HEADER { 0xFA, 0x4E, 0x02, 0x00, 0x10, 0x00, 0xB8, 0x20, 0x18, 0x00 }
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/*
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get timeval using simulation time
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@ -91,15 +86,6 @@ void VectorNav::send_packet1(void)
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struct VN_packet1 pkt {};
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struct timeval tv;
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simulation_timeval(&tv);
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if (start_us == 0) {
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start_us = tv.tv_usec * 1000;
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}
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pkt.timeStartup = start_us;
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pkt.timeGPS = tv.tv_usec * 1000;
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pkt.uncompAccel[0] = fdm.xAccel;
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pkt.uncompAccel[1] = fdm.yAccel;
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pkt.uncompAccel[2] = fdm.zAccel;
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@ -115,6 +101,9 @@ void VectorNav::send_packet1(void)
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pkt.mag[0] = fdm.bodyMagField.x*0.001;
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pkt.mag[1] = fdm.bodyMagField.y*0.001;
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pkt.mag[2] = fdm.bodyMagField.z*0.001;
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pkt.uncompMag[0] = pkt.mag[0];
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pkt.uncompMag[1] = pkt.mag[1];
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pkt.uncompMag[2] = pkt.mag[2];
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pkt.accel[0] = fdm.xAccel;
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pkt.accel[1] = fdm.yAccel;
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@ -122,9 +111,6 @@ void VectorNav::send_packet1(void)
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pkt.gyro[0] = radians(fdm.rollRate + rand_float() * gyro_noise);
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pkt.gyro[1] = radians(fdm.pitchRate + rand_float() * gyro_noise);
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pkt.gyro[2] = radians(fdm.yawRate + rand_float() * gyro_noise);
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// pkt.sensSat = ???
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// pkt.AHRSStatus = ???
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pkt.ypr[0] = fdm.yawDeg;
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pkt.ypr[1] = fdm.pitchDeg;
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@ -135,14 +121,6 @@ void VectorNav::send_packet1(void)
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pkt.quaternion[2] = fdm.quaternion.q4;
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pkt.quaternion[3] = fdm.quaternion.q1;
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pkt.linAccBody[0] = fdm.xAccel;
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pkt.linAccBody[1] = fdm.yAccel;
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pkt.linAccBody[2] = fdm.zAccel;
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// pkt.yprU[3] = attitude uncertainty
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// pkt.INSStatus = ??
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pkt.positionLLA[0] = fdm.latitude;
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pkt.positionLLA[1] = fdm.longitude;
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pkt.positionLLA[2] = fdm.altitude;
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@ -187,7 +165,6 @@ void VectorNav::send_packet2(void)
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// pkt.GPS1DOP =
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pkt.numGPS2Sats = 18;
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pkt.GPS2Fix = 3;
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// pkt.GPS2DOP =
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const uint8_t header[] VN_PKT2_HEADER;
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@ -203,6 +180,19 @@ void VectorNav::send_packet2(void)
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write_to_autopilot((char *)&crc2, sizeof(crc2));
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}
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void VectorNav::nmea_printf(const char *fmt, ...)
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{
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va_list ap;
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va_start(ap, fmt);
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char *s = nmea_vaprintf(fmt, ap);
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va_end(ap);
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if (s != nullptr) {
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write_to_autopilot((const char*)s, strlen(s));
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free(s);
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}
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}
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/*
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send VectorNav data
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*/
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@ -222,5 +212,13 @@ void VectorNav::update(void)
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last_pkt2_us = now;
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send_packet2();
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}
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// Strictly we should send this in responce to the request
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// but sending it occasionally acheaves the same thing
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if (now - last_type_us >= 1000000) {
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last_type_us = now;
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nmea_printf("$VNRRG,01,VN-300-SITL");
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}
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}
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@ -43,9 +43,11 @@ public:
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private:
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uint32_t last_pkt1_us;
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uint32_t last_pkt2_us;
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uint32_t last_type_us;
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void send_packet1();
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void send_packet2();
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void nmea_printf(const char *fmt, ...);
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uint64_t start_us;
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};
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