A study of self-guidance algoritm for aircraft in respect of hypersonic aerial objects
Control systems
Аuthors
,Abstract
an analysis of introduced self-guidance algorithm that allows of very manoeuvre hypersonic objects interception is carried out. The results of efficiency and responsibility investigations of algorithm under the conditions of measuring instruments errors while very manoeuvre hypersonic aim striking are presented. The investigations were carried out with simulation. Findings of carried out investigations including possibility of hypersonic objects striking and influences of application conditions and measuring instruments by accuracy of control signal forming. Moreover the measuring accuracy requirements are formulated.Keywords:
self-guidance algorithm, hypersonic aircrafts, the statistical optimum control system theory, the response of guidance algorithm, aviation self-guidance system.Download