uavcan.equipment.air_data.StaticPressure.h 3.6 KB

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  1. #pragma once
  2. #include <stdbool.h>
  3. #include <stdint.h>
  4. #include <canard.h>
  5. #define UAVCAN_EQUIPMENT_AIR_DATA_STATICPRESSURE_MAX_SIZE 6
  6. #define UAVCAN_EQUIPMENT_AIR_DATA_STATICPRESSURE_SIGNATURE (0xCDC7C43412BDC89AULL)
  7. #define UAVCAN_EQUIPMENT_AIR_DATA_STATICPRESSURE_ID 1028
  8. #if defined(__cplusplus) && defined(DRONECAN_CXX_WRAPPERS)
  9. class uavcan_equipment_air_data_StaticPressure_cxx_iface;
  10. #endif
  11. struct uavcan_equipment_air_data_StaticPressure {
  12. #if defined(__cplusplus) && defined(DRONECAN_CXX_WRAPPERS)
  13. using cxx_iface = uavcan_equipment_air_data_StaticPressure_cxx_iface;
  14. #endif
  15. float static_pressure;
  16. float static_pressure_variance;
  17. };
  18. #ifdef __cplusplus
  19. extern "C"
  20. {
  21. #endif
  22. uint32_t _uavcan_equipment_air_data_StaticPressure_encode(struct uavcan_equipment_air_data_StaticPressure* msg, uint8_t* buffer
  23. #if CANARD_ENABLE_TAO_OPTION
  24. , bool tao
  25. #endif
  26. );
  27. bool _uavcan_equipment_air_data_StaticPressure_decode(const CanardRxTransfer* transfer, struct uavcan_equipment_air_data_StaticPressure* msg);
  28. static inline uint32_t uavcan_equipment_air_data_StaticPressure_encode(struct uavcan_equipment_air_data_StaticPressure* msg, uint8_t* buffer
  29. #if CANARD_ENABLE_TAO_OPTION
  30. , bool tao
  31. #endif
  32. ) {
  33. return _uavcan_equipment_air_data_StaticPressure_encode(msg, buffer
  34. #if CANARD_ENABLE_TAO_OPTION
  35. , tao
  36. #endif
  37. );
  38. }
  39. static inline bool uavcan_equipment_air_data_StaticPressure_decode(const CanardRxTransfer* transfer, struct uavcan_equipment_air_data_StaticPressure* msg) {
  40. return _uavcan_equipment_air_data_StaticPressure_decode(transfer, msg);
  41. }
  42. #if defined(CANARD_DSDLC_INTERNAL)
  43. static inline void __uavcan_equipment_air_data_StaticPressure_encode(uint8_t* buffer, uint32_t* bit_ofs, struct uavcan_equipment_air_data_StaticPressure* msg, bool tao);
  44. static inline bool __uavcan_equipment_air_data_StaticPressure_decode(const CanardRxTransfer* transfer, uint32_t* bit_ofs, struct uavcan_equipment_air_data_StaticPressure* msg, bool tao);
  45. void __uavcan_equipment_air_data_StaticPressure_encode(uint8_t* buffer, uint32_t* bit_ofs, struct uavcan_equipment_air_data_StaticPressure* msg, bool tao) {
  46. (void)buffer;
  47. (void)bit_ofs;
  48. (void)msg;
  49. (void)tao;
  50. canardEncodeScalar(buffer, *bit_ofs, 32, &msg->static_pressure);
  51. *bit_ofs += 32;
  52. {
  53. uint16_t float16_val = canardConvertNativeFloatToFloat16(msg->static_pressure_variance);
  54. canardEncodeScalar(buffer, *bit_ofs, 16, &float16_val);
  55. }
  56. *bit_ofs += 16;
  57. }
  58. /*
  59. decode uavcan_equipment_air_data_StaticPressure, return true on failure, false on success
  60. */
  61. bool __uavcan_equipment_air_data_StaticPressure_decode(const CanardRxTransfer* transfer, uint32_t* bit_ofs, struct uavcan_equipment_air_data_StaticPressure* msg, bool tao) {
  62. (void)transfer;
  63. (void)bit_ofs;
  64. (void)msg;
  65. (void)tao;
  66. canardDecodeScalar(transfer, *bit_ofs, 32, true, &msg->static_pressure);
  67. *bit_ofs += 32;
  68. {
  69. uint16_t float16_val;
  70. canardDecodeScalar(transfer, *bit_ofs, 16, true, &float16_val);
  71. msg->static_pressure_variance = canardConvertFloat16ToNativeFloat(float16_val);
  72. }
  73. *bit_ofs += 16;
  74. return false; /* success */
  75. }
  76. #endif
  77. #ifdef CANARD_DSDLC_TEST_BUILD
  78. struct uavcan_equipment_air_data_StaticPressure sample_uavcan_equipment_air_data_StaticPressure_msg(void);
  79. #endif
  80. #ifdef __cplusplus
  81. } // extern "C"
  82. #ifdef DRONECAN_CXX_WRAPPERS
  83. #include <canard/cxx_wrappers.h>
  84. BROADCAST_MESSAGE_CXX_IFACE(uavcan_equipment_air_data_StaticPressure, UAVCAN_EQUIPMENT_AIR_DATA_STATICPRESSURE_ID, UAVCAN_EQUIPMENT_AIR_DATA_STATICPRESSURE_SIGNATURE, UAVCAN_EQUIPMENT_AIR_DATA_STATICPRESSURE_MAX_SIZE);
  85. #endif
  86. #endif