We present results of development and practical implementation of the adaptive correction method and algorithm. They ensure high accuracy and stability of the airborne low-frequency inductive electromagnetic measurements. We describe the theoretical foundations of the method and the basic schemes of the algorithm, and consistently consider the stages of computational transformations. We provide several examples of experimentally obtained data proving the effectiveness of the method. The main result achieved is the possibility of functioning of the airborne electromagnetic system without calibration during the entire flight.