Abstract Discrete-event drag-modulation trajectory control is assessed for planetary entry using the closed-form Allen-Eggers solution to the equations of motion. A control authority metric for drag-modulation trajectory control systems is derived. Closed-form analytical relationships are developed to assess range divert capability and to identify jettison condition constraints for limiting peak acceleration and peak heat rate. Closed-form relationships are also developed for drag-modulation systems with an arbitrary number of stages.
Analytical Assessment of Drag-Modulation Trajectory Control for Planetary Entry
2018
Article (Journal)
English
Analytical Assessment of Drag-Modulation Trajectory Control for Planetary Entry
Springer Verlag | 2018
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