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    Basic Information

Technology developed: Novel Gear Based Actuation Mechanism for Spacecrafts Attitude Control Focused on Fault-tolerance (TP19765061398)
Category: Product(Hardware/Material/Software)
Details of Inventor(s):
Inventor Institution/Organization/Company Department Designation
Priyank Dubey IIT Kanpur AE Research Associate
Dipak Kumar Giri IIT Kanpur AE Professor
Technical Application Area: Aviation
If 'Other', please specify:
Please give more details of new technical application area:
Organization(s):
Indian Institute of Technology (IIT) Kanpur
Affiliated Ministry: Ministry of Education
Type of technology development: Indigenous
Does the technology help in replacing any import items currently
procured from outside India?
Yes
Does the technology have export potential? Yes
Category of Technology developed: Immediate Deployment
Stage of Development: Field Test
Please describe in detail including the TRL Level:
The plan is being executed

    Abstract:

Applications: A new concept of gear based Multi-Motor Mono-Reaction Wheel System (MMMRWS) actuation mechanism for spacecraft attitude control is designed with the capability of autonomously tolerating the multiple actuator failures, while simultaneously reducing the size of spacecraft. The spacecraft Attitude Control is an integral subsystem of spacecraft control which orients and maintains the desired state in spite of disturbance torques and other perturbations acting on the spacecraft. The linking of single reaction wheel with multiple motors in the proposed MMMRWS autonomously handle the multiple actuator failures onboard, provides mechanical advantages and further reducing the size of satellite or spacecraft
Advantages: With the increasing demand and a great market for small satellites for various missions like Earth observation, weather monitoring, space exploration, military, communications, navigation and science applications, search and rescue. Spacecraft needs to reliable, they should have capability of autonomously tolerating the faults onboard without any human intervention. Further miniaturization of spacecraft has always been desired as small satellite require smaller and cheaper launch vehicles and can sometimes be launched in multiples, can be used in formations to gather data from multiple points, in-orbit inspection of larger satellites, university-related research, testing or qualifying new hardware before using it on a more expensive spacecraft. The designed ACS will help to construct the satellites which can autonomously tolerate the multiple actuator failures onboard without compromising the expensive mission. It can also further reduce the size of satellite or spacecraft

    Technology Inputs:

Imported Equipment/Spare Parts:
Equipment/Spare Parts Year ITC-HS Code
NA
Indigenous Equipment/Spare Parts:
Equipment/Spare Parts Year ITC-HS Code
NA
Imported Raw Materials:
Raw Materials Year ITC-HS Code
NA
Indigenous Raw Materials:
Raw Materials Year ITC-HS Code
NA
Existing R&D Facilities used:
Facilities Year ITC-HS Code
NA

   Patents & Publications:

Patents:
Filed Patents (No.) Granted Patents (No.) Year
1 0 2020-21
Publications:
Submitted (No.) Published (No.) Year
0 0 NA

    Commercialization Potential:

Who are the Potential Licensees?
What commercially available products address
the same problem?
Company Product Problem Addressed
Would you like to develop this invention further with
corporate research support?
Yes
Would you be interested in participating in cluster based
programs for commercialization research or business
planning for your invention?
Yes
      Submitted by: J.G. Rao Date of Submission: 5-5-2022



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