This paper presents a cyclic pursuit based strategy for monitoring a stationary target with multiple autonomous vehicles. The strategy needs only bearing angle information of the target and that of only one of the nei...
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This paper considers the problem of controlling relative attitude between two spacecrafts, so as to follow a smoothly time varying desired relative attitude trajectory. The spacecrafts are modelled as rigid bodies and...
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Motion planning of an autonomous robot in an unknown environment is a challenging task. The prerequisite of any motion planning task is collision avoidance. This paper aims on designing a steering control-law for cons...
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In this paper a guidance law has been proposed to solve applications related to coverage of a pre-defined area using a mobile robot. In many situations, it may not be possible to measure all the information due to pra...
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This paper, investigates the one of open problems of robust controller design for discrete fractional order system. For achieving the specified goal a disturbance observer is constructed based on full state informatio...
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The Stewart platform manipulator is a 6 degrees of freedom parallel robot with a superior performance over serial robots. A variable gain super twisting algorithm ensuring global finite time convergence to the desired...
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The paper proposes a method for determining energy optimal trajectory from source position to goal position for differential drive robots. Energy consumption depends on the velocity profile of the generated trajectory...
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This paper presents a cyclic pursuit based strategy for monitoring a stationary target with multiple autonomous vehicles. The strategy needs only bearing angle information of the target and that of only one of the nei...
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This paper presents a cyclic pursuit based strategy for monitoring a stationary target with multiple autonomous vehicles. The strategy needs only bearing angle information of the target and that of only one of the neighbor vehicle. We have considered simple kinematic model for each vehicle. With the proposed control law, at equilibrium the vehicles get into a rigid polygonal formation which rotates around the target. The stability of equilibrium formations is analyzed using linearization technique. The effectiveness of the proposed strategy is demonstrated through simulation.
This paper deals with the development and analysis of fractional-order (FO) point reactor kinetics (FPRK) model with reactivity feedback for a nuclear reactor. Incorporation of adiabatic temperature feedback of reacti...
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This paper considers the problem of controlling relative attitude between two spacecrafts, so as to follow a smoothly time varying desired relative attitude trajectory. The spacecrafts are modelled as rigid bodies and...
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This paper considers the problem of controlling relative attitude between two spacecrafts, so as to follow a smoothly time varying desired relative attitude trajectory. The spacecrafts are modelled as rigid bodies and attitudes are represented in non-linear state space of SO(3). The attitude control law proposed does not need relative attitude measurement and is determined from line of sight (LOS) unit vectors measured by spacecrafts to each other and from each spacecraft to a common object in respective body fixed frames. Unlike existing control laws using LOS measurements, positions of spacecrafts are not considered fixed. The state feedback laws proposed in this work guarantee almost global asymptotic tracking of the desired time varying attitude trajectory, when positions of spacecrafts do not become collinear or coincide. The simulation results of the proposed control law are also shown.
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