Nonlinear vector model control of underactuated air cushion vehicle based on parameter reduction algorithm

Author(s):  
Shuang Gao ◽  
Jingjing Xue

Due to the serious drift phenomenon of underactuated air cushion vehicle, the actual trajectory is determined by the total speed and course angle. In this paper, the course angle and total speed model are derived from the general four degrees of freedom air cushion vehicle model and named nonlinear vector model. Nonlinear vector model can be used to directly design the course and total speed controllers for underactuated air cushion vehicle. Adaptive radial basis function neural network is introduced to deal with the strong nonlinearity and uncertainty of air cushion vehicle’s complex dynamics. However, the adaptive weights to be calculated and updated may be too many in each sampling period. For the relief of the burden caused by the online computing, parameter reduction algorithm is designed in this paper. It gives us a power to choose the number of online update parameters freely. Then the new trajectory tracking control method with independent total speed and course controller is designed based on nonlinear vector model and parameter reduction algorithm. The designed controller ensures that the tracking errors are uniformly ultimately bounded. Also, only a few weights need to be updated online. The effectiveness and superiority of the designed controller is verified by simulation results.

2020 ◽  
Vol 42 (14) ◽  
pp. 2733-2743
Author(s):  
Jiqiang Tang ◽  
Tongkun Wei ◽  
Qichao Lv ◽  
Xu Cui

For a magnetically suspended control moment gyro (MSCMG), which is an ideal attitude actuator for its large outputting control moment and fast response, the moving-gimbal effects due to the coupling between the moving gimbal and high-speeding rotor will make the magnetically suspended rotor (MSR) unstable. To improve control precision, both the dynamic model of MSR and the feedback linearization control are done to decouple tilting motion, and poles of the system are reconfigured to reduce control error. To suppress the varying disturbance moments caused by moving-gimbal effects, an extended state observer (ESO) is originally designed to estimate and compensate them timely and accurately. To improve system robustness, a two-degree freedom internal model control (2-DOF IMC) is researched to suppress model error. Compared with existing proportional integral derivative (PID) control method, simulations done on a single gimbal MSCMG with 200 N.m.s angular momentum indicated that this presented control method with ESO and 2-DOF IMC can suppress the moving-gimbal effects more effectively and make the rotor suspension more stable.


Author(s):  
А. Г. Гребеников ◽  
В. П. Люшнин ◽  
Т. Б. Богачева ◽  
Л. А. Мальков

In the modern world, the task of rapid delivery of goods and passengers between cities and countries is an urgent task. The "atmospheric" transport system is proposed as an alternative to the Hyperloop vacuum system in the form of an air cushion vehicle moving at a speed of 500 km / h over an overpass with an arch cover. Structurally, the device is designed as a cargo option for the rapid delivery of sea containers, and in the passenger version. The design of the device is simplified, and the risks associated with depressurization in a vacuum environment are excluded. The proposed transport is environmentally friendly and not dependent on the weather conditions of the environment. Methods are described that allow to determine the characteristics of air cushions, the parameters of the vehicle's movement along a curved path, as well as traction and energy indicators. Calculations are made on a concrete example.


1975 ◽  
Vol 12 (3-4) ◽  
pp. 201-216 ◽  
Author(s):  
R.Wingate Hill

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