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  • session 3

    Title

    Navigation, Guidance and Control for Deep Space Missions - Session 3

    type

    oral

    Description

    This Track will address topics dedicated to Navigation, Guidance and Control for Deep Space Missions: Interplanetary Trajectory Design and Optimization; Attitude Determination and Control; Deep Space Communication and Tracking; Precision Landing and Hazard Avoidance; Simulation and Testing of Navigation Systems; etc.

    Date

    2025-05-09

    Time

    14:30

    Room

    Room 403

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    14:30

    Fuel Optimal, Explicit Guidance Law for Powered Descent Guidance on Mars

    15'

    confirmed

    Mrs. Sunanda Lona

    Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram

    India

    2

    14:45

    The development of an energy and information transmission system utilizing the conductive elements of transformable space antennas

    15'

    confirmed

    Mr. Fedor Mitin

    Baltic State Technical University VOENMEH

    Russian Federation

    3

    15:00

    Real-Time DEM Refinement for Autonomous Space Exploration

    15'

    confirmed

    Mr. KRISHNAN LAKSHMI NARAYANA

    Indian Institute of Technology, Madras

    India

    4

    15:15

    A Novel Location and Attitude Determination System for a Swarm of High-Speed Martian Tumbleweed Rovers

    15'

    confirmed

    Dr. Tolga Ors

    Team Tumbleweed

    United Kingdom

    5

    15:30

    Quantum-Enhanced Autonomous Navigation for Deep Space: A Feasibility Study on Entanglement-Based Positioning and Ultra-Precision Orientation Systems

    15'

    confirmed

    Mr. TEJAS NARESH REDDY

    AgniKul Cosmos

    India

    6

    15:45

    Aditya-L1: ISRO’s First Solar Mission — Flight Dynamics Operations until Halo Orbit Insertion

    15'

    confirmed

    Mrs. Litty Jose

    ISRO

    India

    7

    16:00

    Development of an integrated framework for perception, planning and control of space missions

    15'

    confirmed

    Mr. Karthik R

    Vikram Sarabhai Space Centre (VSSC)

    India

    8

    16:15

    Trajectory Design for L2 Halo Orbits in the Sun-Earth System: Utilizing Invariant Manifolds with Radiation Pressure and Oblateness Effects

    15'

    confirmed

    Ms. Abhistha Singh

    SRM Institute of Science and Technology

    India