The invention discloses a standard trajectory tracking guidance method based on a height-range ratio. The method comprises the steps of 1, determining the total range of an aircraft and an aircraft height and speed corridor under constraint conditions; 2, designing a guidance law instruction of a segmentation constant value, and recording the guidance law instruction as u (h); 3, obtaining terminal ranges f1 and f2 in a prediction correction method formula; 4, calculating a gain k, a parameter h *, a range f *, and an updating parameter tau on the premise of an approximate linearization hypothesis, ; 5, carrying out n times of iterative computation to obtain a time sequence of theheight-range ratio; 6, when the reentry vehicle is subjected to external interference in the flight process, and the initial condition is uncertain, improving the guidance precision through the correction value delta u of the control quantity; and 7, forming a guidance law instruction form when the reentry vehicle is subjected to external interference and initial conditions are uncertain. In order to solve the problem of standard trajectory tracking of an under-actuated reentry vehicle system, longitudinaland lateral planes are combined, and the concept of height-range ratio is introduced to solve the problem.