Skip to main content
Log in

Performance evaluation of multi-sensor data-fusion systems in launch vehicles

  • Published:
Sadhana Aims and scope Submit manuscript

Abstract

In this paper, the utilization of multi-sensors of different types, their characteristics, and their data-fusion in launch vehicles to achieve the goal of injecting the satellite into a precise orbit is explained. Performance requirements of sensors and their redundancy management in a typical launch vehicle are also included. The role of an integrated system level-test bed for evaluating multi-sensors and mission performance in a typical launch vehicle mission is described. Some of the typical simulation results to evaluate the effect of the sensors on the overall system are highlighted

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  • Chidambaram T R, Sivan K, Sudar I, Sreelatha A 1996a Integrated flight software validation for launch vehicle mission.Proc. National Workshop on Flight Software (Thiruvananthapuram: Systems Society of India) pp. 4.1–4.14

    Google Scholar 

  • Chidambaram T R, Sivan K, Lal V B, Sudar I, Sreelatha A 1996b Hardware-in-loop simulations for testing inertial guidance system elements of launch vehicle.J. Aerosp. Soc. India 48: 331–337

    Google Scholar 

  • Chidambaram T R, Sivan K, Sudar I 2002 Integrated testing of inertial navigation systems of launch vehicle.Proc. National Workshop on Navigation Systems — Present scenario and future trends (Thiruvananthapuram: Systems Society of India)

    Google Scholar 

  • Gupta A K, Sajeendran 2002 Test and calibration systems for inertial sensors.Proc. National Workshop on Navigation Systems — Present scenario and future trends (Thiruvananthapuram: Systems Society of India)

    Google Scholar 

  • Puri S N 2002 Navigation system development and its performance for GSLV-D1 mission.Proc. National Workshop on Navigation Systems — Present scenario and future trends (Thiruvananthapuram: Systems Society of India)

    Google Scholar 

  • Shukkoor A A, Bhattacharyya K C, Gopakumar S, Hemachandran S, Santha Kumari K K, Syamala S 2000 Simulation testing of strapdown inertial navigation system and software.Proc. National Workshop on Aerospace Flight Simulation (Thiruvananthapuram: Systems Society of India)

    Google Scholar 

  • Sivan K, Sreelatha A, Chidambaram T R 2000a Integrated validation of navigation, guidance and control systems of launch vehicles through simulations.Proc. National Workshop on Aerospace Flight Simulation (Thiruvananthapuram: Systems Society of India)

    Google Scholar 

  • Sivan K, Lal V B, Sudar I, Chidambaram T R 2000b Simulation facilities for validating navigation, guidance and control system of launch vehicles.Proc. National Workshop on Aerospace Flight Simulation (Thiruvananthapuram: Systems Society of India)

    Google Scholar 

  • Sivan K, Sudar I, Sreelatha A, Chidambaram T R 2000c Actuator-in-loop simulation for validating satellite launch vehicle navigation, guidance and control systems.Proc. 24th National Systems Conference, Bangalore, pp. 62–73

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Suresh, B.N., Sivan, K. Performance evaluation of multi-sensor data-fusion systems in launch vehicles. Sadhana 29, 175–188 (2004). https://doi.org/10.1007/BF02703730

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02703730

Keywords

Navigation