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contributor authorNash, Austin L.
date accessioned2022-12-27T23:21:54Z
date available2022-12-27T23:21:54Z
date copyright8/18/2022 12:00:00 AM
date issued2022
identifier issn2689-6117
identifier otheraldsc_2_3_031010.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4288477
description abstractImpact point prediction, estimation, and control is a critical component of many smart weapons applications. In this work, I propose a method for estimating and controlling impact points of indirect fire launches for a spin-stabilized symmetric projectile with forward-mounted canard actuators. My method uses an algebraic point mass model to enable parameter estimation for time-varying parameters within a separate linear prediction model that can be leveraged for real-time impact point control. The point mass model also serves as the basis for a reference trajectory for any launch condition and thus eliminates the need for obtaining preloaded reference trajectories. I then use a linear prediction model in conjunction with the parameter estimates to synthesize a linear MPC tracking control algorithm for projectile impact point control. The MPC tracking controller allows incorporation of actuator saturation constraints and is shown to successfully guide a set of indirect fire launches toward a desired downrange target. A comparative case study to existing work in the literature shows that the proposed method results in a 56% reduction in the CEP radius, which is a prescribed radius such that half of the points of a given set lie within the circle, for a set of 50 yaw and pitch launch angle pairs.
publisherThe American Society of Mechanical Engineers (ASME)
titleModel Predictive Tracking Control With Parameter Estimation for Spin-Stabilized Indirect Fire Symmetric Projectiles
typeJournal Paper
journal volume2
journal issue3
journal titleASME Letters in Dynamic Systems and Control
identifier doi10.1115/1.4055124
journal fristpage31010
journal lastpage31010_8
page8
treeASME Letters in Dynamic Systems and Control:;2022:;volume( 002 ):;issue: 003
contenttypeFulltext


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