aerospace systems
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2022 ◽  
Author(s):  
Roberto Furfaro ◽  
Andrea D'Ambrosio ◽  
Enrico Schiassi ◽  
Andrea Scorsoglio

2022 ◽  
Author(s):  
Vikram Shyam ◽  
Paht Juangphanich ◽  
Ezra O. McNichols ◽  
Brooke Weborg ◽  
Herbert Schilling ◽  
...  

Author(s):  
Ilya Kolmanovsky ◽  
Marija Ilić
Keyword(s):  

AIAA Journal ◽  
2021 ◽  
pp. 1-12
Author(s):  
Pier Carlo Berri ◽  
Matteo D. L. Dalla Vedova ◽  
Laura Mainini

Astrodynamics ◽  
2021 ◽  
Vol 5 (3) ◽  
pp. 185-215
Author(s):  
Renhe Shi ◽  
Teng Long ◽  
Nianhui Ye ◽  
Yufei Wu ◽  
Zhao Wei ◽  
...  

AbstractThe design of complex aerospace systems is a multidisciplinary design optimization (MDO) problem involving the interaction of multiple disciplines. However, because of the necessity of evaluating expensive black-box simulations, the enormous computational cost of solving MDO problems in aerospace systems has also become a problem in practice. To resolve this, metamodel-based design optimization techniques have been applied to MDO. With these methods, system models can be rapidly predicted using approximate metamodels to improve the optimization efficiency. This paper presents an overall survey of metamodel-based MDO for aerospace systems. From the perspective of aerospace system design, this paper introduces the fundamental methodology and technology of metamodel-based MDO, including aerospace system MDO problem formulation, metamodeling techniques, state-of-the-art metamodel-based multidisciplinary optimization strategies, and expensive black-box constraint-handling mechanisms. Moreover, various aerospace system examples are presented to illustrate the application of metamodel-based MDOs to practical engineering. The conclusions derived from this work are summarized in the final section of the paper. The survey results are expected to serve as guide and reference for designers involved in metamodel-based MDO in the field of aerospace engineering.


Author(s):  
Ekansh Pradhan ◽  
◽  
Aman Dadheech ◽  
Himanshu Agarwal ◽  
Taruna Singh ◽  
...  

Advancements in technology in the fields of satellite and aerospace systems and the need for smaller yet efficient designs have paved the way for further research into nano and pico-satellites. Smaller systems can prove to be more economical in investigating and measuring various parameters of the atmosphere in a localized area. This paper aims to demonstrate the design of one such system. A can-sized satellite (CanSat) has been designed with respect to the restrictions imposed by the CanSat Competition 2020. The design is developed in a way that allows it to be lightweight without compromising structural integrity. The manufacturing technique aimed to be used is 3D printing using Polylactic Acid (PLA) which allows for greater flexibility in customization and ease of fabrication. The application areas of the model satellite range from space exploration to weather forecasting.


2021 ◽  
Vol 31 (1) ◽  
pp. 816-831
Author(s):  
Eric van Velzen ◽  
Alison Olechowski

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