The invention relates to a close-range intersection trajectory
robust control method in multi-target tracking, relates to an
optimal control problem analysis objective function, constraint establishment and robust approach
trajectory control scheme, and belongs to the field of
spacecraft situation awareness and control. The method comprises the following steps: firstly, establishing an
optimal trajectory control problem, and comprehensively considering
information gain and security constraints to establish a model basis of a
robust control instruction; and secondly, by establishing an analytical expression of a Hellinger distance in an
optimal control problem under an OPMs (Out Probability Measurement) theory, effectively evaluating a difference between prior
estimation and posteriori
estimation of a target state, and further calculating
information gain values under different control instructions so as to screen out an
optimal control instruction. Meanwhile, by establishing an upper and lower bound analysis expression of the void probability in the optimal control problem constraint condition under the OPMs theory, the void probability of the rendezvous trajectory at any moment under different control instructions can be efficiently calculated, so that the safety of the rendezvous trajectory is evaluated, and the control instructions meeting the constraint condition are screened out. And finally, designing a robust
trajectory control module and a possibility
label multi-Bernoulli filtering module, forming a close-range rendezvous trajectory
robust control scheme, and realizing the target of generating an optimal control instruction in real time in the approaching and tracking process so as to achieve the effects of maximizing
information gain and ensuring the rendezvous trajectory safety.