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  • IAC-26
  • D2
  • IP
  • session IP

    Title

    Interactive Presentations - IAF SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM

    type

    interactive

    Description

    This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Space Transportation Solutions and Innovations addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific ten minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the D Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.

    Room

    IP Area

    IPC members
    • Co-Chair: Dr. Ysolde PREVEREAUD, ONERA - The French Aerospace Lab, France;

    • Co-Chair: Dr. Jens Lassmann, ArianeGroup, Germany;

    • Rapporteur: Dr. Aaron Weaver, National Aeronautics and Space Administration (NASA), United States;

    papers

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    A Sub-Optimal Staging Method for Usage in Pre-Conceptual Design of Launch Vehicles

    confirmed

    Dr. Ahmet Sofyalı

    ROKETSAN Roket Sanayi ve Ticaret A.S.

    Türkiye

    A Guidance Algorithm for Suborbital Vehicle Powered Descent Phase Based on Improved Convex Optimization

    confirmed

    Dr. Hang Hu

    CAS Space

    China

    hybrid hardware in the loop validation for sounding rocket active roll control under limited infrastructure

    confirmed

    Mr. Jose Maria Piñera Diaz

    Instituto Politécnico Nacional

    Mexico

    Sustainable Space Transportation: Versatile Deployable Sail Spacecraft

    confirmed

    Ms. Zitong Bai

    School of Astronautics, Beihang University

    China

    DESIGN PROCESS FOR A TELEMETRY SYSTEM AS A PAYLOAD FOR THE PERUVIAN SOUNDING ROCKET PAULET 1-D

    confirmed

    Mr. George Steve Fajardo Soria

    Agencia Espacial del Peru (CONIDA)

    Peru

    Adaptive finite-time control considering elastic frequency identification and suppression for flexible near-space high-speed vehicles

    confirmed

    Mr. Xuebao Ma

    Northwestern Polytechnical University

    China

    Aerodynamic Response of a Slender Rocket Across Mach 0.3–1.2 Under Free-Flight and Near-Surface Conditions

    Dr. Baris Gungordu

    Middle East Technical University

    Cyprus

    Combined attitude controller tuning and control system actuator optimization for a small rapid response launcher

    confirmed

    Mr. Hao Gu

    Beihang University

    China

    A Unified Convexification Paradigm for Multi-Segment Trajectory Planning with Time-Varying Dynamics

    confirmed

    Mr. Shuzhao Chen

    LandSpace Technology Corporation Ltd.

    China

    Design, development and flight testing of a student-built sounding rocket with a sloshing dynamics payload

    confirmed

    Ms. iclal emine BALTA

    Türkiye

    Development of a Modular Suborbital Validation Platform for Incremental TRL (3-5) Advancement of Student-Built Avionics Systems

    confirmed

    Mr. Angel Vázquez

    High Technology Unit (UAT) Faculty of Engineering - UNAM

    Mexico

    Development of Scalable Suborbital Rocket Platforms for Atmospheric Intervention and Cloud Microphysics Applications in the Andean Region

    confirmed

    Mr. Rodrigo Augusto Martinez Chavez

    University of California, Berkeley

    United States

    Implementation-Oriented Analysis of Sliding Mode Control for Vertical Landing Rockets with Actuator Feasibility Constraints

    confirmed

    Ms. Ayşe Sultan ŞAHİNCİ

    Kırklareli University

    Türkiye

    Numerical Investigation of Aerodynamic Characteristics for a Novel Reusable Rocket First Stage During High-Angle-of-Attack Reentry

    Dr. haohuan han

    Beihang University (BUAA)

    China

    RELIABLE AND EFFICIENT TRAJECTORY OPTIMIZATION FOR THE FULL-FLIGHT LANDING OF STARSHIP-LIKE VEHICLES

    confirmed

    Dr. Cong Zhou

    Zhejiang University

    China

    Trajectory Optimization of a Suborbital Carrier Vehicle for High-Altitude Solar UAV Release

    Mr. Zhan Zuo

    Beijing AZSPACE Technology Co., Ltd

    China

    A hybrid model-data-driven reentry guidance method based on sequential optimal trajectory sets

    confirmed

    Ms. Yelin Liu

    Northwestern Polytechnical University

    China

    Transformers Enable Rapid Aerodynamic Model Identification for Launch Vehicles with Actuator Dynamics

    confirmed

    Mr. Shuyue Fu

    Beihang University (BUAA)

    China

    Transonic Aerodynamic Instability and Supersonic Stability Analysis of a Mach 1.4 Suborbital Rocket

    confirmed

    Mr. Erhan Şencan

    Turkish Technology Team Foundation

    Türkiye

    Innovative Application of Digital Tube Templating Technology in the ZQ-3 Launch Vehicle

    confirmed

    Mr. Zhen Li

    LandSpace Technology Corporation Ltd.

    China