Work

Real-Time Retargeting-Based Robust Polynomial Guidance for Chandrayaan-3 Lunar Landing Mission

Year: 2026

Type: article

Source: Journal of Guidance Control and Dynamics

DOI: 10.2514/1.g008733

Authors: Suraj Kumar, Debajyoti Chakrabarti, Aditya Rallapalli, G. V. P. Bharat Kumar

Institution: Indian Space Research Organisation

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W7140143111

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Cites: 31

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