Job description

Details of work:
  • Design, implement, test, and validate algorithms used in the AOCS Synthetic Aperture Radar (SAR) satellites, such as: sensor data filtering, orbit and attitude estimation, attitude controller, reaction wheels and magnetorquer control, operation modes control, failsafe mechanisms, etc.
  • Work closely with the embedded software engineers to integrate the AOCS into the rest of the flight software.
  • Validate the design through unit testing, Model In the Loop Simulation (MILS), Hardware In the Loop Simulation (HILS), and tests on the physical satellite.
  • Assist the testing and validation of the AOCS components during the satellite Assembly Integration and Testing (AIT) process.
  • Model sensors, actuators, and other physical components in MATLAB/Simulink/Simscape and fit the component model using test data.
  • Take part in the launch campaign: prepare the necessary items for launch operation, monitor the behavior during the critical phase, and provide technical support to the satellite operation team.
  • Participate in weekly meetings and design reviews.
  • Perform design studies for the development of our next generation of satellites.
  • Review and validate designs and test results.
  • Mentor more junior members.
Selling points of the role:
  • Great opportunity for growth as an engineer.
  • See the complete lifecycle of a satellite, from the early design to the launch and in-orbit operation.
  • Work in an international team.

Requirements

Job requirements
  • Bachelor’s degree in Aerospace Engineering, Control Engineering, Electrical Engineering, or Robotics Engineering. We will consider an equivalent combination of relevant education and/or experience.
  • At least 8 years of hands-on experience in the design and validation of control systems, preferably on autonomous systems (satellite, launch vehicle, drone, Unmanned Aerial Vehicle (UAV), self-driving car, robot, etc.).
  • Thorough understanding of multibody dynamics: coordinate transformation between reference frames, kinematics, conservation of energy and momentum, etc.
  • Strong analytical and communication skills.
  • Strong experience with MATLAB/Simulink.
  • Experience working with physical sensors and actuators.
  • Willingness to travel to Synspective's factory (Yamato-city) on business trips several times a year.
Preferred qualifications:
  • Knowledge of orbital mechanics and satellite dynamics.
  • Experience in the design, implementation and testing of spacecraft attitude and orbit control algorithms.
  • Experience in modeling physical components such as sensors and actuators in MATLAB/Simulink.
  • Experience in control law design, beyond classical techniques: non-linear design, optimal design.
  • Experience in state estimation using Kalman filtering and anomaly detection algorithms.
  • Experience in model identification.
  • Knowledge of GNC hardware components such as: reaction wheels, magnetorquers, GPS receivers, gyroscopes, star trackers.
  • Experience in modeling finite state machines in Stateflow.
  • Experience programming in C/C++.
  • Experience in generating C/C++ code from Simulink.

Job details

Job type
Full time
Job category
IT
Job location
Tokyo
Salary
¥9,000,000 ~ ¥10,000,000
Language requirement
English (Business advanced)
Industry
Information Technology
Working hours
9:00 - 18:00
Probation period
3 months

About the company

Our client is a spacetech start-up that utilizes data to offer business solutions.


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