Control Allocation Strategies for a Hybrid Controlled Missile with NDI Autopilot

Date

2022-01-01

Author

Biyikli, Rabiya
Tekin, Raziye
Yavrucuk, İlkay

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This study presents roll angle, lateral, and longitudinal acceleration autopilots for a highly agile air defense missile with both aerodynamic tail control and thrust vector control (TVC) parts. Nonlinear Dynamic Inversion (NDI) is studied to handle bank-to-turn and agile maneuvers due to the cross-coupling effects. Output redefinition is implemented using the center of percussion idea for the nonminimum phase of the tail-controlled missiles. Another arduous feature of the system is that the dual control of the system generates a need to allocate the control between aerodynamic and thrust control. Driving aerodynamic fins and jet vanes with the same actuator is found preferable for some systems that creates a mechanically coupled or, in other words, integrated design. Further, this paper shows the effect of allocating control with or without this mechanical coupling.

Subject Keywords

aerodynamic control, air defense missile, coupled dynamics, nonlinear dynamic inversion, thrust vector control

URI

https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85135601743&origin=inward
https://hdl.handle.net/11511/101385

DOI

https://doi.org/10.23919/ascc56756.2022.9828187

Conference Name

13th Asian Control Conference, ASCC 2022

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

R. Biyikli, R. Tekin, and İ. Yavrucuk, “Control Allocation Strategies for a Hybrid Controlled Missile with NDI Autopilot,” presented at the 13th Asian Control Conference, ASCC 2022, Jeju, Güney Kore, 2022, Accessed: 00, 2023. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85135601743&origin=inward.