Missile guidance and pursuit
N.A. Shneydor
- 01 Jan 1998
392
About: The article was published on 01 Jan 1998. The article focuses on the topics: Missile guidance & Pursuit guidance.
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Citations
Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints
TL;DR: In this paper, the authors proposed guidance laws to intercept targets at a desired impact angle, from any initial heading angle, without exhibiting any singularity, by selecting interceptor's lateral acceleration to enforce nonsingular terminal sliding mode on a switching surface designed using nonlinear engagement dynamics.
356
Internal models direct dragonfly interception steering
TL;DR: By simultaneously tracking the position and orientation of a dragonfly’s head and body during flight, this work provides evidence that interception steering is driven by forward and inverse models of dragonfly body dynamics and by models of prey motion.
316
Impact Angle Constrained Interception of Stationary Targets
Ashwini Ratnoo,Debasish Ghose +1 more
TL;DR: In many advanced guidance applications, it is required to intercept the target from a particular direction, that is, achieve a certain impact angle as discussed by the authors. But this is not the case in our case.
296
Modified Pure Proportional Navigation Guidance Law for Impact Time Control
Namhoon Cho,Youdan Kim +1 more
TL;DR: In this paper, an analytic solution for the time-to-go of the pure proportional navigation guidance law against a stationary target is derived considering full nonlinear engagement kinematics without near-collision course approximation.
182
References
Optimal Stochastic Guidance Laws for Tactical Missiles
John J. Deyst,Charles F. Price +1 more
TL;DR: In this paper, the authors developed guidance laws for tactical missiles which take into account the following important dynamic and random effects: random target motion, homing sensor measurement noise, bounded control level, bounded acceleration level, and missile autopilot dynamics.
28
On Pursuit with Curvature Constraints
TL;DR: In this article, it was shown that the pursuer can, without violating constraints, keep the line of sight parallel to the original and ultimately collide with the evader, provided the pursuers have greater speed and greater normal acceleration.
27
Optimal biased proportional navigation
S. Brainin,Robert B. McGhee +1 more
TL;DR: It is shown that the addition of an appropriate bias term to a proportional navigation guidance equation allows an interceptor missile to attain an efficiency which can be made to approach that of an optimum system.
27
Bat-like sonar for guiding mobile robots
Roman Kuc,Billur Barshan +1 more
TL;DR: Simulations and experiments with real mobile robots show that both capture probability and mean capture time are inversely related to the prey/pursuer speed ratio, and demonstrate that bat-like sonar represents an efficient sensing system.
25