1981
DOI: 10.2514/3.56061
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Comparison of Optimal Control and Differential Game Intercept Missile Guidance Laws

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Cited by 92 publications
(27 citation statements)
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“…To date, guidance theories have been commonly used as a means to efficiently, with minimal computational burden, navigate interceptors toward targets with unpredictable trajectories, first in missile-guidance applications [1][2][3], and more recently, in mobile robotics [4][5][6][7]. The roboticguidance techniques proposed in the literature have been shown to clearly yield improved interception times when compared to classical visual-servoing techniques.…”
Section: Introductionmentioning
confidence: 99%
“…To date, guidance theories have been commonly used as a means to efficiently, with minimal computational burden, navigate interceptors toward targets with unpredictable trajectories, first in missile-guidance applications [1][2][3], and more recently, in mobile robotics [4][5][6][7]. The roboticguidance techniques proposed in the literature have been shown to clearly yield improved interception times when compared to classical visual-servoing techniques.…”
Section: Introductionmentioning
confidence: 99%
“…Missileguidance laws assume that the future trajectory of the target is completely defined either analytically or by a probabilistic model [5][6][7]. However, the problem of velocity matching, as Faraz Kunwar and Beno Benhabib, Advanced Predictive Guidance Navigation for Mobile Robots:…”
Section: A Guidance-based Interceptionmentioning
confidence: 99%
“…Many ongoing researches are still focused on PN-related topics, such as the Augmented Proportional Navigation (APN) laws [10], spiraling related laws (here spiraling means a periodic conical pitching and yawing motion) [12][13][14][15], time-varying effective navigation ratio [11], etc. These extensions advance PN along different directions and are suitable for different situations.…”
Section: Fig 1 Missile Interception Illustrationmentioning
confidence: 99%
“…Under relatively loose constraints [17][18], theoretically, DGL/1 can reduce the final miss to zero without the drawbacks of the saturation in the optimal feedback control solution. [10,[19][20], although theoretically DGL/1 should be "better than" them. For this reason, DGL/1's and its guidance laws are not used in existing antimissile products.…”
Section: Fig 1 Missile Interception Illustrationmentioning
confidence: 99%