The invention discloses an inertial navigation assisted
Big Dipper single-frequency whole-cycle
ambiguity calculation method under the short baseline condition. The inertial navigation assisted
Big Dipper single-frequency whole-cycle
ambiguity calculation method comprises three steps of firstly conducting grouping difference on
Big Dipper observed quantity according to the height of a Big
Dipper constellation type
orbit, wherein
atmosphere delay errors of the Big
Dipper observed quantity under the short baseline condition can be effectively eliminated; secondly, utilizing an inertial navigation output attitude matrix to estimate a baseline vector and substituting a baseline vector into a Big
Dipper double-difference carrier wave observation equation, utilizing a recursive least-squares method to calculate whole-cycle
ambiguity floating point solution and a
covariance matrix of the
floating point solution, then adopting an improved least-squares ambiguity de-
correlation method to fix a whole-cycle ambiguity integer solution; finally, utilizing an inertial navigation estimated baseline vector and a Big Dipper three-difference
carrier phase observed value to produce inspection amount so as to judge whether a
cycle slip occurs or not, estimating and repairing a
cycle slip value if the
cycle slip occurs. By means of the inertial navigation assisted Big Dipper single-frequency whole-cycle ambiguity calculation method under the short baseline condition, the calculation speed and accurate of the whole-cycle ambiguity can be effectively improved, and the method is suitable for positioning and attitude fixing of a high-dynamic carrier under the condition of a single-frequency Big Dipper
satellite system.