English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Global: Zendy Plus annual

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Global: Zendy Tools annual

Global: Zendy Free Plan

Global: Zendy Tools monthly

Global: Zendy Plus monthly

The size and weight of Satellites are currently being miniaturised in order to meet the purpose of lowering cost and saving production time. For this situation, a type of Small-Satellite known as the CubeSat has been identified. This kind of small-satellite is 10 cm 3 cube of less than 1.33kg. Due to its limitations on overall ma ss and dimensions, the CubeSat uses nanotechnology components for the interior design. Therefore, an appropriate design is a crucial aspect of any CubeSat project. According to space vehicle research and development criteria, the simulation and modelling of the subsystems of CubeSat is both significant and necessary. This paper investigates a feasibility study and demonstrates the simulation of Small-Satellite orbital navigation determination and Propulsion system modelling.

Small-satellite propulsion system modelling and simulation of orbital navigation determination; A feasibility study