Spacecraft Attitude Control
Pontryagin's Maximum Principle is a fundamental result in optimal control theory that provides necessary conditions for optimality in control problems. It establishes that the optimal control can be characterized as maximizing a Hamiltonian function, which incorporates both the system dynamics and the cost associated with the control inputs. This principle is essential for designing effective control strategies, especially when dealing with linear-quadratic regulators (LQR) that require an optimal solution to minimize a quadratic cost function.
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