IR focal plane array seekers for ground-to-ground and air-to-ground missiles

Riedl, Guenther; Assel, Michael; Fendt, A.; Hetzer, Walter; Keller, Erwin; Kilger, Fridbert; Kuligk, Thomas; Popp, Ludwig; Proels, Rudolf; Schweyer, Nikolaus

doi:10.1117/12.445304

Cited by 6 publications

(2 citation statements)

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“…2, it is the relative motion diagram for missile and target. Define [4]: x z y y x x z z q x y z x z…”

Section: A Mass Center Of Missile Motion Equationmentioning

confidence: 99%

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Research on Improved Extended Proportional Navigation Guidance

Feng¹,

Yang²,

Yao³

et al. 2013

AMM

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This paper proposed an improved method on the basis of the extended proportional guidance law. The method solved the weak observability problem of system sate in guided missile attacking maneuvering target. It is simple in form and easy for engineering implementation. This paper set up relative motion model and the observability theory indexes. The improved propotional guidance law is simulated using the MATLAB language. The simulation results show that the method is reasonable, effective and improving the observability.

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“…2, it is the relative motion diagram for missile and target. Define [4]: x z y y x x z z q x y z x z…”

Section: A Mass Center Of Missile Motion Equationmentioning

confidence: 99%

“…In order to watch the ideal trajectory, it assumes that the target was maneuvering flight in space (4,3,4) The missile attacks the target in the space (0, 0, 0). N=3, 0.6 / m v km s =…”

Section: Simulation and Analysismentioning

confidence: 99%