2022
DOI: 10.3390/aerospace9070356
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Fixed-Time Circular Impact-Time Guidance with Look Angle Constraint

Abstract: A fixed-time nonlinear circular guidance law that satisfies the impact time constraint is proposed. By utilizing the geometric principle that the length of a circular arc connecting the missile and the target can be analytically calculated, the exact expression of time-to-go is obtained. Thus, the impact time error can be shaped to zero, and the missile can intercept the target at the desired time, which is crucial in a salvo attack. The settling time of the impact time error is proved to be bounded by a fixed… Show more

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Cited by 5 publications
(1 citation statement)
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“…Moreover, to satisfy impact time constraint, guidance gains or parameters are often tuned by trial and error, or by using an optimization routine, which can make on-line calculations less efficient. In addition, a fixed-time nonlinear circular guidance law that satisfies the impact time constraint is proposed in [24]. Using the geometric principle that the length of a circular arc connecting the air vehicle and the object can be analytically calculated, the exact expression of time-to-go can be obtained.…”
Section: Introductionmentioning
confidence: 99%
“…Moreover, to satisfy impact time constraint, guidance gains or parameters are often tuned by trial and error, or by using an optimization routine, which can make on-line calculations less efficient. In addition, a fixed-time nonlinear circular guidance law that satisfies the impact time constraint is proposed in [24]. Using the geometric principle that the length of a circular arc connecting the air vehicle and the object can be analytically calculated, the exact expression of time-to-go can be obtained.…”
Section: Introductionmentioning
confidence: 99%