The invention discloses a strapdown inertial navigation attitude
algorithm precision evaluation method. A polynomial coefficient is set according to a required carrier dynamic environment; according to the polynomial, calculating attitude truth values of all time needing reference in an off-line manner; deriving an
angular velocity analytical expression according to the attitude
truth value, and generating
gyroscope observation; the method comprises the following steps: taking
gyroscope observation as input of a strapdown inertial navigation attitude
algorithm to be evaluated, updating attitude parameters of a carrier, and obtaining an attitude calculation result; after each attitude
algorithm is solved, the algorithm performance is quantitatively evaluated; after each algorithm performance evaluation, adjusting parameters and a
coefficient matrix of the attitude trajectory model or storing current
evaluation data; and storing the adjusted
model parameters or
evaluation data, and when a new high-order attitude algorithm needs to be verified or a maneuvering scene needs to be further expanded, turning to the initial step and sequentially carrying out recursive iteration until an evaluation task is completed. According to the method, large-angle maneuvering scene
simulation and attitude /
angular velocity analysis
truth value acquisition can be considered, and the high-order attitude algorithm performance can be verified more accurately and efficiently.