Development of navigation guidance and control technology for Indian launch vehicles |
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Authors: | S C Gupta B N Suresh |
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Affiliation: | (1) Vikram Sarabhai Space Centre (VSSC), 695 022 Trivandrum, India |
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Abstract: | The orbital injection accuracy of any payload depends on the calibre of the inertial guidance system used on board the launch
vehicle. This paper outlines the mission definition and the rationale for the selection of a proper guidance system to meet
final mission objectives. The functions and the architecture of the navigation, guidance and control are discussed. The developmental
aspects of the sophisticated inertial sensors, inertial systems, associated complex electronics, on-board computers, control
actuators and systems are reported. The complexity of the on-board control and guidance software and the test and evaluation
procedures used for their validation are included. The general scheme of the inertial guidance systems and the critical role
played by them in the realization of Indian satellite launch vehicles SLV-3, ASLV and PSLV are presented in brief. |
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Keywords: | Inertial guidance navigation vehicle flexibility stabilized platform strap-down system control algorithm hardware-in-loop simulation |
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