Abstract
To meet the growing energy demand of the new spacecraft such as high resolution and radar remote sensing satellite and deep space probes, a incremental conductance peak power tracking method based on S3MPR circuit is presented in this paper. The shortcomings of traditional MPPT topology that low mass and power ratio, low efficiency are overcome. The incremental conductance method can be used to reduce the oscillation near the maximum power point. The principle and control processes of the incremental conductance method are introduced. A co-simulation platform and semi-physical experimental platform is built to validate the circuit and control method. The results show, the incremental conductance peak power tracking method based on S3MPR circuit can achieve effective tracking of the maximum power point of the solar array, and has good tracking efficiency, the simulation and experiment platform are reasonable and effective.
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsReferences
Miao D (2011) Improved dynamic response power density and integrated topology research on power condition unit of spacecraft (in Chinese)
Ding L (2012) Research on micro-satellite power systems and related ground test equipment. Zhejiang University, Zhejiang (in Chinese)
Yan W, Xu W (2011) Analysis and comparison about power regulating technology. Aerospace Dongfanghong Satellite Co. Ltd., Beijing, 1–5(in Chinese)
Brambilla A, Gambarara M, Torrente G (2002) Perturb and observe digital maximum power point tracker for satellites applications. In: Proceedings of the sixth European space power conference. ESA, Paris, pp 263–268
Ebale G, Lamantia A, La Bella M (2005) Power control system for the AGILE satellite. In: Seventh European space power conference. ESA, Paris, pp 589–596
Garrigos A, Blanes JM, Carrasco JA et al (2007) The sequential switching shunt maximum power regulator and its application in the electric propulsion system of a spacecraft. In: Power electronics specialists conference. IEEE, New York, pp 1374–1379
Xu P, Liu F, Liu B et al (2007) Analysis, comparison and improvement of several MPPT methods for PV system. Power Electron 5(41):3–5 (in Chinese)
He W, Yu X, Yang J et al (2009) Photovoltaic maximum power point tracking system based on an improved MPPT algorithm. Electric Drive 6(39):39–41
Liu Z, Cai Z, Chen Q et al (2011) Overview of space power system design using MPPT for deep space spacecraft. Spacecraft Engineer 20(5):105–110 (in Chinese)
Lin W, Liu Z, Ma L (2013) Simulation of maximum power point tracking digital control based on optimized gradient method. Spacecraft Engineer 22(4):82–86 (in Chinese)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Du, Q. et al. (2020). Research of Space Power System MPPT Topology and Algorithm. In: Liang, Q., Wang, W., Liu, X., Na, Z., Jia, M., Zhang, B. (eds) Communications, Signal Processing, and Systems. CSPS 2019. Lecture Notes in Electrical Engineering, vol 571. Springer, Singapore. https://doi.org/10.1007/978-981-13-9409-6_203
Download citation
DOI: https://doi.org/10.1007/978-981-13-9409-6_203
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-13-9408-9
Online ISBN: 978-981-13-9409-6
eBook Packages: EngineeringEngineering (R0)