Desensitized Aerocapture Terminal Guidance

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Authors: Pardhasai Chadalavada, Rohan G. Deshmukh, Soumyo Dutta, Ehsan Taheri
Cited by: 0
References: 24

Abstract

In traditional aerocapture terminal guidance, feedback gains are computed with respect to a nominal optimal trajectory determined a priori. In contrast, desensitized aerocapture terminal guidance simultaneously optimizes both the reference trajectory and feedback gains by minimizing sensitivity terms that depend on the feedback gains themselves. Previous studies have demonstrated that aerocapture performance exhibits significant sensitivity to uncertainties in atmospheric density and initial state conditions, particularly initial velocity and flight-path angle. This study develops a desensitized aerocapture terminal guidance approach designed to enhance robustness against dynamic perturbations. The performance and robustness of the desensitized aerocapture terminal guidance is evaluated through Monte Carlo analysis conducted within the Program to Optimize Simulated Trajectories-II (POST2).

Fields of Study & Subjects

Spacecraft Dynamics and Control Guidance and Control Systems Space Satellite Systems and Control

Publication details

Journal / source
AIAA SciTech Forum
Publication date
8 January 2026