Results 61 to 70 of about 75,283 (193)
Time-Varying Biased Proportional Guidance with Seeker’s Field-of-View Limit
International Journal of Aerospace Engineering, 2016 Traditional guidance laws with range-to-go information or time-to-go estimation may not be implemented in passive homing missiles since passive seekers cannot measure relative range directly.
Zhe Yang, Hui Wang, Defu Lin
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Minimum-fuel turning climbout and descent guidance of transport jets [PDF]
The complete flightpath optimization problem for minimum fuel consumption from takeoff to landing including the initial and final turns from and to the runway heading is solved.
Kreindler, E., Neuman, F.
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IEEE Access, 2019 This paper proposes an integral sliding mode guidance law with the constraints of the line-of-sight angle and its rate for the interception of a non-cooperative maneuvering target.
Yan Xiaodong, Lyu Shi
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Relative Geodesics in the Special Euclidean Group
, 2013 We propose a notion of distance between two parametrized planar curves, called their discrepancy, and defined intuitively as the minimal amount of deformation needed to deform the source curve into the target curve. A precise definition of discrepancy is
Holm, Darryl D. +2 more
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Defence Technology, 2014 A new guidance law, called biased retro proportional navigation (BRPN), is proposed. The guidance law is designed to intercept high-speed targets with angular constraint, which can be used for ballistic target interception.
Liang Yan +3 more
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Intercepting Higher-Speed Targets Using Generalized Relative Biased Proportional Navigation
Xibei Gongye Daxue Xuebao, 2019 To intercept a higher-speed target in the terminal guidance phase, this paper proposes a generalized relative biased proportional navigation (BPN) law. In order to enlarge the capture domain of the classical proportional navigation (PN) law and make full
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Approximate Optimal Atmospheric Entry Trajectories [PDF]
Approximate optimal atmospheric entry trajectories maximizing terminal function of velocity, heading angle, flight path angle, and ...
Speyer, J. L., Womble, E.
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Aerodynamic preliminary analysis system. Part 2: User's manual and program description [PDF]
A comprehensive aerodynamic analysis program based on linearized potential theory is described. The solution treats thickness and attitude problems at subsonic and supersonic speeds.
Divan, P., Dunn, K., Kojima, J.
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A study of the application of singular perturbation theory [PDF]
A hierarchical real time algorithm for optimal three dimensional control of aircraft is described. Systematic methods are developed for real time computation of nonlinear feedback controls by means of singular perturbation theory. The results are applied
Carroll, J. V. +3 more
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Adaptive Sliding Mode Guidance Law with Terminal Angle Constraint [PDF]
Advances in Intelligent Systems Research, 2015 Suochang Yang, Kuanqiao Zhang
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