2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC) 2018
DOI: 10.1109/gncc42960.2018.9018887
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Decoupling ADRC Lateral/Directional Controller of Autonomous Carrier-based UAV Landing

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Cited by 3 publications
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“…After linearizing Equation ( 1) with small perturbations, the state space equation of the control system can be obtained as shown in Equation ( 2 2) is the basic equation of motion for the longitudinal landing of a carrier aircraft. For a better simulation of the actual flight, the dynamics of the elevator and throttle should be considered when designing the controller [9] . The dynamics of the F/A-18A actuator can be represented by Equations ( 3) and ( 4).…”
Section: Iscme-2022mentioning
confidence: 99%
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“…After linearizing Equation ( 1) with small perturbations, the state space equation of the control system can be obtained as shown in Equation ( 2 2) is the basic equation of motion for the longitudinal landing of a carrier aircraft. For a better simulation of the actual flight, the dynamics of the elevator and throttle should be considered when designing the controller [9] . The dynamics of the F/A-18A actuator can be represented by Equations ( 3) and ( 4).…”
Section: Iscme-2022mentioning
confidence: 99%
“…Gao Yang [8] et al designed a robust and coordinated decoupling control strategy based on high-order LADRC for vertical/short takeoff and landing aircraft and simulated it to verify the effectiveness and robustness of the strategy. Wu Wenhai [9] et al proposed a transverse lateral decoupled ADRC landing control method for naval UAVs subject to lateral naval wake interference and severe coupling and verified the method with good tracking performance, robustness, and anti-disturbance.…”
Section: Introductionmentioning
confidence: 99%