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Guidance command assumed is the lateral acceleration (latax), applied normal to the velocity vector.
After each guidance cycle, the guidance command updates the trajectory using the actual states obtained from the control design.
The main idea of this paper is to use LM as a design parameter for shaping the guidance command as well as controlling the terminal constraints.
Results show that the sliding guidance provides a more robust solution in off-nominal scenarios while providing similar fuel consumption when compared to the non-sliding guidance command.
The guidance command of CSGL-LM is given a unified functional form of the time-to-go, the state variables, and LM.
The proposed optimal trajectory technique satisfies the mission constraints in each phase and provides an overall fuel-minimizing guidance command history.
Similar(45)
Firstly, the feasible guidance strategy is proposed to obtain the desired guidance commands.
It leads to smooth guidance commands to fulfill the terminal line of sight angle constraint.
A nonlinear modelbased controller is designed for a fully actuated vessel to enable it to comply with the guidance commands.
The control design is found to track the guidance commands well for perturbations in the initial reentry conditions.
The equilibrium glide condition and an exponential function of altitude are used to parameterize the guidance commands of two portions and generate the guidance sequence.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com