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Grant: Discovery Grants Program - Individual

Toronto Metropolitan University

$25,000.00

New Paradigm for Spacecraft Control and Design Technologies

FY 2022-23

Summary
The proposed research "New Paradigm for Spacecraft Control and Design" will focus on developing next generation of low cost, autonomous and intelligent spacecraft. The research will be conducted under four main areas: 1) Harnessing Environmental Forces for Spacecraft Control, 2) Robust Control or Fault Tolerant Control Methodologies for Spacecraft, 3) Novel Actuators for Spacecraft Control, and 4) Spacecraft Design, Miniaturization and Hardware Innovation. The first objective involves harnessing environmental forces efficiently for spacecraft control (simple called "Propellant-less Spacecraft Control") while the second objective focuses on fault diagnosis, prognosis and control to develop intelligent controllers for a swarm of spacecraft. In addition, it also focuses on big data analytics for spacecraft health management. On the other hand, the third objective involves the development of novel actuators for spacecraft control including fluid rings, tethers and MEMS (piezoelectric). The fourth objective involves spacecraft design with a focus on ultra small satellites, such as attosatellites (1 - 10g). Finally, the developed algorithms will be integrated into spacecraft hardware and tested on high-fidelity system models and spacecraft formation platforms available in Dr. Kumar's Space Systems Dynamics and Control laboratory. The proposed research will lead to the development of intelligent high performance spacecraft for future space missions as well as training of a large number of HQPs (6 PhD students, 9 MASc students, and 4 Undergraduate research assistants) in the most demanding areas of system modelling and simulation, big data analytics, sensors, actuators, software development, and hardware design.
Program
Discovery Grants Program - Individual
Location
Ontario, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data

As published

Application id
RGPIN-2017-05534
Name nom
Kumar, Krishna
Department département
Aerospace Engineering - Aerospace Engineering
Organization id
43
Institution établissement
Toronto Metropolitan University
Province en
Ontario
Province fr
Ontario
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2022
Competition year année de concours
2017
Award amount
25000
Program id
RGPIN
Program name en
Discovery Grants Program - Individual
Program name fr
Programme de subventions à la découverte - individuelles
Group en
DISCOVERY RESEARCH
Group fr
RECHERCHE AXÉE SUR LA DÉCOUVERTE
Committee code
1512
Committee name en
Mechanical Engineering
Committee name fr
Génie mécanique
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2100
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Mechanical engineering
Research subject fr
Génie mécanique
Installment
inst:6
Partie
1
Nb partie
6
Application title
New Paradigm for Spacecraft Control and Design Technologies
Application summary
The proposed research "New Paradigm for Spacecraft Control and Design" will focus on developing next generation of low cost, autonomous and intelligent spacecraft. The research will be conducted under four main areas: 1) Harnessing Environmental Forces for Spacecraft Control, 2) Robust Control or Fault Tolerant Control Methodologies for Spacecraft, 3) Novel Actuators for Spacecraft Control, and 4) Spacecraft Design, Miniaturization and Hardware Innovation. The first objective involves harnessing environmental forces efficiently for spacecraft control (simple called "Propellant-less Spacecraft Control") while the second objective focuses on fault diagnosis, prognosis and control to develop intelligent controllers for a swarm of spacecraft. In addition, it also focuses on big data analytics for spacecraft health management. On the other hand, the third objective involves the development of novel actuators for spacecraft control including fluid rings, tethers and MEMS (piezoelectric). The fourth objective involves spacecraft design with a focus on ultra small satellites, such as attosatellites (1 - 10g). Finally, the developed algorithms will be integrated into spacecraft hardware and tested on high-fidelity system models and spacecraft formation platforms available in Dr. Kumar's Space Systems Dynamics and Control laboratory. The proposed research will lead to the development of intelligent high performance spacecraft for future space missions as well as training of a large number of HQPs (6 PhD students, 9 MASc students, and 4 Undergraduate research assistants) in the most demanding areas of system modelling and simulation, big data analytics, sensors, actuators, software development, and hardware design.
Toronto Metropolitan University - $25,000 Grant (2022… | Canada Spends