Abstract
This chapter proposes a new trajectory shaping guidance law for impact time control and impact angle control with seeker’s field-of-view (FOV) limit. The proposed guidance law is derived by using the concept of biased PNG (BPNG). The guidance law developed leverages a nonlinear function to ensure the boundedness of velocity lead angle to cater for seeker’s FOV constraint. The finite-time convergence of the impact time error and impact angle error is theoretically analyzed. By investigating the optimality of the biased command, the physical meaning of the proposed trajectory shaping guidance law is revealed to support practical applications. Numerical simulations clearly demonstrate the effectiveness of the proposed formulation.
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References
Sang DK, Tahk M-J (2009) Guidance law switching logic considering the seeker’s field-of-view limits. Proc Inst Mech Eng, Part G: J Aerosp Eng 223(8):1049–1058
Shim S-W, Hong S-M, Moon G-H, Tahk M-J (2018) Impact angle and time control guidance under field-of-view constraints and maneuver limits. Int J Aeronaut Space Sci 19(1):217–226
Saleem A, Ratnoo A (2016) Lyapunov-based guidance law for impact time control and simultaneous arrival. J Guid, Control, Dyn 39(1):164–173
Jeon I-S, Lee J-I (2017) Impact-time-control guidance law with constraints on seeker look angle. IEEE Trans Aerosp Electron Syst 53(5):2621–2627
Zarchan P (2012) Tactical and strategic missile guidance. American Institute of Aeronautics and Astronautics
Kim H-G, Kim HJ (2016) Impact time control guidance considering seeker’s field-of-view limits. In 2016 IEEE 55th Conference on Decision and Control (CDC). IEEE, pp 4160–4165
Lee C-H, Kim T-H, Tahk M-J (2013) Interception angle control guidance using proportional navigation with error feedback. J Guid, Control, Dyn 36(5):1556–1561
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He, S., Lee, CH., Shin, HS., Tsourdos, A. (2020). Optimal Trajectory Shaping Guidance Law with Seeker’s Field-of-View Constraint. In: Optimal Guidance and Its Applications in Missiles and UAVs. Springer Aerospace Technology. Springer, Cham. https://doi.org/10.1007/978-3-030-47348-8_3
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DOI: https://doi.org/10.1007/978-3-030-47348-8_3
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