2008
DOI: 10.1007/s10883-008-9047-7
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Optimal Attitude Control of a Rigid Body Using Geometrically Exact Computations on SO(3)

Abstract: An efficient and accurate computational approach is proposed for optimal attitude control of a rigid body. The problem is formulated directly as a discrete time optimization problem using a Lie group variational integrator. Discrete necessary conditions for optimality are derived, and an efficient computational approach is proposed to solve the resulting two point boundary value problem. The use of geometrically exact computations on SO(3) guarantees that this optimal control approach has excellent convergence… Show more

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Cited by 58 publications
(64 citation statements)
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“…The contribution of the external control moment and the Carnot energy loss term are denoted by u d k and Q d k . They are defined to approximate the additional term in the variational principle (20) that arises due to a discontinuity:…”
Section: Lie Group Variational Integratormentioning
confidence: 99%
See 1 more Smart Citation
“…The contribution of the external control moment and the Carnot energy loss term are denoted by u d k and Q d k . They are defined to approximate the additional term in the variational principle (20) that arises due to a discontinuity:…”
Section: Lie Group Variational Integratormentioning
confidence: 99%
“…These provide a realistic mathematical model for tethered systems and a reliable numerical simulation tool that characterizes the nonlinear coupling between the string dynamics, the rigid body dynamics, and the reel mechanism accurately. The proposed high-fidelity computational framework can be naturally extended to formulating and solving control problems associated with string deployment, retrieval, and vibration suppression as in [20]. This paper is organized as follows.…”
Section: Introductionmentioning
confidence: 99%
“…Then geometric PD controllers on SO(3) and SE(3) were designed and applied on a quadrotor [2,[11][12][13]. Moreover, Lee et al provided the computational optimal geometric method on SO(3) [14,15] and employed the Pontryagin maximum principle to attain solutions of an open loop time-optimal problem. Spindler provided the differential equations which the optimal controls must satisfy via Pontryagin maximum principle.…”
Section: Introductionmentioning
confidence: 99%
“…However, not so many numerical methods are available for solving optimal control problems for dynamical systems whose configuration space is a differentiable manifold. Noticeable and interesting exceptions are the discrete-time methods presented in [12], [13], [14], [15] for mechanical systems on Lie groups. This paper is organized as follows.…”
Section: Introductionmentioning
confidence: 99%