Positioning method, program, positioning device, and electronic apparatus

A positioning method, comprising:

• predicting a state vector including a position of a positioning device and a velocity of the positioning device based on a satellite signal;
• predicting a first reception frequency of the satellite signal;
• measuring a second reception frequency of the satellite signal;
• calculating a velocity of the positioning device based on a difference between the first reception frequency and the second reception frequency;
• predicting a first distance-equivalent value indicating a distance between a positioning satellite and the positioning device;
• measuring a second distance-equivalent value indicating a predicted value of the distance between the positioning satellite and the positioning device;
• calculating an observed value indicating a difference between the first distance-equivalent value and the second distance-equivalent value;
• setting a first measurement error for the positioning satellite based on a signal strength of the satellite signal;
• setting a suitability condition of the observed value based on the calculated velocity;
• setting a second measurement error larger than the first measurement error when the observed value is not suitable by the suitability condition;
• setting the second measurement error equal to the first measurement error when the observed value is suitable by the suitability condition;
• correcting the state vector using the observed value and the second measurement error being larger than the first measurement error, when the observed value is not suitable by the suitability condition;
• and
• correcting the state vector using the observed value and the second measurement error being equal to the first measurement error, when the observed value is suitable by the suitability condition.

A positioning method, comprising:

• predicting a state vector including a position of a positioning device and a velocity of the positioning device based on a satellite signal;
• evaluating a reliability of the satellite signal based on the correlation value by correlating the satellite signal and a replica signal;
• predicting a first distance-equivalent value indicating a distance between a positioning satellite and the positioning device;
• measuring a second distance-equivalent value indicating a distance between the positioning satellite and the positioning device;
• calculating an observed value indicating a difference between the first distance-equivalent value and the second distance-equivalent value;
• setting a first measurement error for the positioning satellite based on a signal strength of the satellite signal;
• setting a suitability condition of the observed value based on the reliability;
• setting a second measurement error larger than the first measurement error when the observed value is not suitable by the suitability condition;
• and
• setting the second measurement error equal to the first measurement error when the observed value is suitable by the suitability condition;
• correcting the state vector using the observed value and the second measurement error being larger than the first measurement error, when the observed value is not suitable by the suitability condition;
• and
• correcting the state vector using the observed value and the second measurement error being equal to the first measurement error, when the observed value is suitable by the suitability condition.