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Considering the full nonlinear point-mass dynamics, a guidance scheme is developed in three-dimensional space.
A guidance scheme designed for coping with significant dispersion in the vehicle's state and atmospheric conditions is presented.
Meanwhile, a guidance scheme is provided to drive the actuator to the position where the observer state reaches the maximum value to improve the control performance.
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A cooperative guidance scheme, where coordination algorithms and local guidance laws are combined together, is proposed.
This paper examines a smart guidance scheme based on Lyapunov feedback control which overcomes the difficulties found in control gains steering.
This paper deals with a near-optimal guidance scheme for a spacecraft flying from a low Earth orbit (LEO) to a low Mars orbit (LMO).
Under such circumstances, a ground vision guidance scheme was proposed and developed [5 11].
This paper describes an efficient optimal guidance scheme for the design of time-optimal and time-fixed fuel-optimal low-thrust spiral trajectories.
Using the recently developed model predictive static programming (MPSP) technique, a nonlinear suboptimal reentry guidance scheme is presented in this paper for a reusable launch vehicle (RLV).
This paper suggests a flatness theory-based guidance scheme dedicated to the Terminal Area Energy Management (TAEM) guidance of a Reusable Launch Vehicle.
A novel closed-loop guidance scheme is designed based on the coupling relationship and unscented kalman filter.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com