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- W4281868149 abstract "Re-entry vehicle (REV) longitudinal autopilot aims the vehicle in order to track guidance commands to reach the required target with minimum miss distance. The trajectory of a ballistic aerospace vehicle from launch to impact point can be divided into three phases of flight: powered, ballistic, and reentry phases. The autopilot of REV will be utilized to control the vehicle motion in the re-entry phase. Aerospace vehicle longitudinal autopilot usually configured as two-loop with PI compensator or three-loop with angular rate and acceleration feedback. In this paper, the static stability problems are studied and compensated by adding a stability augmentation loop in three-loop autopilot structure. A comparative analysis is carried out with the two loop autopilot topology to present the effect of the proposed three loop autopilot structure. The autopilot topologies are presented for a REV linear time invariant (LTI) system model at different design points through re-entry trajectory and The standard control signal algorithm is used to analyse the system using MATLAB/Simulink environment." @default.
- W4281868149 created "2022-06-13" @default.
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- W4281868149 date "2022-03-29" @default.
- W4281868149 modified "2023-09-27" @default.
- W4281868149 title "Re-entry Vehicle Longitudinal Autopilot Design via Two-Loop with PI and Three-Loop Topologies" @default.
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- W4281868149 doi "https://doi.org/10.1109/iceeng49683.2022.9782033" @default.
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