2011Transactions of Beijing Institute of TechnologyRequires access

Autopilot Design of Single Channel Rolling Missile

Xuhui Liu

Open publisher page 1 citations

Abstract

For a single channel rolling missile,the autopilot structure was constructed in body coordinate system.By rolling transfer of coordinate system,the structure loop was transferred to quasi-body coordinate system and was simplified.Then the autopilot structure was designed in quasi-body coordinate system.It is notified that the cross couplings between the vertical and lateral motion exist in the autopilot loop of quasi-body coordinate system.To eliminate the cross couplings,decoupling control of autopilot loop was implemented by means of series compensation.Simulation results prove that the design method presented in this article is feasible.

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What this paper is about

For a single channel rolling missile,the autopilot structure was constructed in body coordinate system.By rolling transfer of coordinate system,the structure loop was transferred to quasi-body coordinate system and was simplified.Then the autopilot structure was designed in quasi-body coordinate system.It is notified that the cross couplings between the vertical and lateral motion exist in the autopilot loop of quasi-body coordinate system.To eliminate the cross couplings,decoupling control of autopilot loop was implemented by means of series compensation.Simulation results prove that the design method presented in this article is feasible.

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Available abstract

For a single channel rolling missile,the autopilot structure was constructed in body coordinate system.By rolling transfer of coordinate system,the structure loop was transferred to quasi-body coordinate system and was simplified.Then the autopilot structure was designed in quasi-body coordinate system.It is notified that the cross couplings between the vertical and lateral motion exist in the autopilot loop of quasi-body coordinate system.To eliminate the cross couplings,decoupling control of autopilot loop was implemented by means of series compensation.Simulation results prove that the design method presented in this article is feasible.

Key concepts: Autopilot, Missile, Control theory (sociology), Decoupling (probability), Coordinate system, Engineering, Control system, Loop (graph theory)

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