Adaptation of pendulum accelerometer compensatory type to perturbing factors of outer space

A method adaptation of the pendulum accelerometer compensation type of the spacecraft control system to the long-term action of perturbing factors of orbital flight is considered. The method is based on the use of self-monitoring techniques pendulum accelerometer compensation type. The method allows to take into account the degradation of the parameters of the components of the accelerometer in conditions of prolonged exposure to space factors.