2021
DOI: 10.1134/s1064230721010123
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Optimization of Automatic Support Systems of Air Objects Based on Local Quadratic-biquadratic Functionals. I. Synthesis of Optimum Control

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Cited by 3 publications
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“…Researchers have made significant contributions to aircraft guidance. New local quadratic-biquadratic quality functions [ 6 ] were used to obtain more general linear-cubic control laws for aircraft guidance. For altitude and position control, in a previous study [ 7 ], incremental nonlinear dynamic inversion control was proposed, which is able to track the desired acceleration of the vehicle across the flight envelope.…”
Section: Introductionmentioning
confidence: 99%
“…Researchers have made significant contributions to aircraft guidance. New local quadratic-biquadratic quality functions [ 6 ] were used to obtain more general linear-cubic control laws for aircraft guidance. For altitude and position control, in a previous study [ 7 ], incremental nonlinear dynamic inversion control was proposed, which is able to track the desired acceleration of the vehicle across the flight envelope.…”
Section: Introductionmentioning
confidence: 99%