2022
DOI: 10.3934/jimo.2021009
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A control parametrization based path planning method for the quad-rotor uavs

Abstract: A time optimal path planning problem for the Quad-rotor unmanned aerial vehicles (UAVs) is investigated in this paper. A 3D environment with obstacles is considered, which makes the problem more challenging. To tackle this challenge, the problem is formulated as a nonlinear optimal control problem with continuous state inequality constraints and terminal equality constraints. A control parametrization based method is proposed. Particularly, the constraint transcription method together with a local smoothing te… Show more

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Cited by 4 publications
(2 citation statements)
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“…By introducing the APF into the procedure of controller design, different control schemes have been proposed to guarantee the feasibility of attitude pointing constraints and the convergence of closed-loop system, such as APF-based proportional and derivative (PD) controller [7,3,9], APF-based backsteping controller [7], and APF-based sliding mode controller [23,15]. The angular velocity and input constrains are also considered in [9] by utilizing optimal control method [17,10,8,2,24,11]. Although most of the existing researches have obtained numerous admirable results for spacecraft attitude maneuver with attitude constraints, it is still a problem when the angular velocity and inertia matrix can not always be measured accurately.…”
mentioning
confidence: 99%
“…By introducing the APF into the procedure of controller design, different control schemes have been proposed to guarantee the feasibility of attitude pointing constraints and the convergence of closed-loop system, such as APF-based proportional and derivative (PD) controller [7,3,9], APF-based backsteping controller [7], and APF-based sliding mode controller [23,15]. The angular velocity and input constrains are also considered in [9] by utilizing optimal control method [17,10,8,2,24,11]. Although most of the existing researches have obtained numerous admirable results for spacecraft attitude maneuver with attitude constraints, it is still a problem when the angular velocity and inertia matrix can not always be measured accurately.…”
mentioning
confidence: 99%
“…Control Paremeterization. In this section, we first introduce the control parameterization (CP) technique [20,21,22,23,24,25,26,27,28,29,30,31] to parameterize the controller U (t) in a sequence, which can easily transform the original optimal control problem into a sequence optimal parameter selection problem. The purpose of this step is to facilitate the design and implementation of our subsequent optimization algorithm.…”
mentioning
confidence: 99%