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Autonomous Navigation System for High Altitude Balloons
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.
2019 (English)Doctoral thesis, comprehensive summary (Other academic)
Place, publisher, year, edition, pages
Luleå tekniska universitet, 2019. , p. 150
Series
Doctoral thesis / Luleå University of Technology 1 jan 1997 → …, ISSN 1402-1544
National Category
Aerospace Engineering
Research subject
Onboard space systems
Identifiers
URN: urn:nbn:se:ltu:diva-76476ISBN: 978-91-7790-486-1 (print)ISBN: 978-91-7790-487-8 (electronic)OAI: oai:DiVA.org:ltu-76476DiVA, id: diva2:1364883
Public defence
2020-01-24, IRF Aula, Kiruna, 09:00 (English)
Opponent
Supervisors
Available from: 2019-10-23 Created: 2019-10-22 Last updated: 2023-01-23Bibliographically approved
List of papers
1. Aerobot design for planetary explorations
Open this publication in new window or tab >>Aerobot design for planetary explorations
2016 (English)In: AIAA Space and Astronautics Forum and Exposition, SPACE 2016, American Institute of Aeronautics and Astronautics, 2016Conference paper, Published paper (Refereed)
Abstract [en]

This paper studies the design of planetary aerobots with different types and shapes under various atmospheric conditions. The design framework and specifications are discussed. The development of a simulation tool is described, which is used for analyzing the behaviour of aerobots on Venus, Mars and Titan. The software is verified through the comparison of its performance with some experimental data as well as the state-of-the-art simulation tools. Based on the simulation results, some recommendations are made for different aerobot exploration missions

Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics, 2016
National Category
Other Electrical Engineering, Electronic Engineering, Information Engineering
Research subject
Onboard space systems
Identifiers
urn:nbn:se:ltu:diva-60882 (URN)10.2514/6.2016-5448 (DOI)2-s2.0-85076210424 (Scopus ID)
Conference
AIAA Space and Astronautics Forum and Exposition, SPACE 2016, Long Beach, 13-15 September 2016
Note

ISBN för värdpublikation: 978-162410427-5

Available from: 2016-12-02 Created: 2016-12-02 Last updated: 2022-03-14Bibliographically approved
2. Fuzzy Modelling of Zero-pressure Balloon Ascent
Open this publication in new window or tab >>Fuzzy Modelling of Zero-pressure Balloon Ascent
2018 (English)In: 2018 Modeling and Simulation Technologies Conference, 2018Conference paper, Published paper (Refereed)
Abstract [en]

Zero-pressure balloon ascent prediction is a critical issue for Swedish Space Corporation(SSC) as targeted test ights are important part of SSC activities. This paper introducesa data-driven approach for estimating the balloon ascent. An output-constrained fuzzylogic approach is applied to the zero-pressure balloon data set from the past 10 years fromEsrange Space Center and rules are formulated that can express the balloon ascent. Theserules are veried by performing a root mean square analysis of estimated ascent againstthe real ascent trajectory. The result shows that the proposed fuzzy model is reliable andis able to estimate the balloon ascent with an acceptable accuracy.

National Category
Other Electrical Engineering, Electronic Engineering, Information Engineering
Research subject
Onboard space systems
Identifiers
urn:nbn:se:ltu:diva-73399 (URN)10.2514/6.2018-3753 (DOI)2-s2.0-85051630074 (Scopus ID)
Conference
2018 Modeling and Simulation Technologies Conference, June 25-29 2018, Atlanta, Georgia.
Available from: 2019-04-03 Created: 2019-04-03 Last updated: 2022-03-14Bibliographically approved
3. Balloon design for Mars, Venus, and Titan atmospheres
Open this publication in new window or tab >>Balloon design for Mars, Venus, and Titan atmospheres
2020 (English)In: Applied Sciences, E-ISSN 2076-3417, Vol. 10, no 9, article id 3204Article in journal (Refereed) Published
Abstract [en]

This paper studies the specifications of balloons for the exploration of bodies with different atmospheric conditions. Three types of balloons, i.e., zero-pressure, super-pressure, and over-pressurized, with four different shapes, i.e., sphere, oblate, prolate, and airship, were analysed. First, the development of a simulation tool is described, which was used for analysing the behaviour of balloons for different exploration missions. Next, the developed software was verified by comparing its output with recorded data from a set of flights at the Esrange Space Center. Based on the simulation results, recommendations are given for different balloon types and shapes for operation on Mars, Venus, and Titan.

Place, publisher, year, edition, pages
MDPI, 2020
Keywords
balloon, Mars, Venus, Titan, zero-pressure, super-pressure, over-pressurized zero-pressure
National Category
Engineering and Technology Aerospace Engineering
Research subject
Onboard space systems; Atmospheric science
Identifiers
urn:nbn:se:ltu:diva-76541 (URN)10.3390/app10093204 (DOI)000535541900217 ()2-s2.0-85085083322 (Scopus ID)
Funder
Swedish National Space Board, 3941025
Note

Validerad;2020;Nivå 2;2020-06-25 (alebob)

Available from: 2019-10-28 Created: 2019-10-28 Last updated: 2022-03-14Bibliographically approved
4. Wind Based Navigation for Zero-Pressure Stratospheric Balloons Using Reinforcement learning
Open this publication in new window or tab >>Wind Based Navigation for Zero-Pressure Stratospheric Balloons Using Reinforcement learning
2019 (English)In: Acta Astronomica, ISSN 0001-5237Article in journal (Refereed) Submitted
Abstract [en]

The horizontal motion of the balloon is governed by the winds at the float altitude. In order to navigate, and change the direction of balloon flight, knowledge of the wind environment around the balloon is needed. The real time navigation and control of zero-pressure balloons is a challenging task as there are no sensors that can be used onboard the balloon to provide real knowledge of the wind environment. Further, their is no active actuation possible and the resources available for passive actuation are limited. These constraints makes the balloon flight difficult and inflexible. In this paper, a solution to this problem of balloon navigation, and its path planning is presented by using data from ECMWF in combination with reinforcement learning. Data from ECMWF gives an overview of almost real-time environment and a reinforcement learning algorithm help in optimizing the passive actuation resources.

Keywords
Reinforcement learning, balloon, Stratospheric winds
National Category
Aerospace Engineering
Research subject
Onboard space systems
Identifiers
urn:nbn:se:ltu:diva-76542 (URN)
Funder
Swedish National Space Board, 3941025
Available from: 2019-10-28 Created: 2019-10-28 Last updated: 2022-03-14

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Garg, Kanika

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