Tatiya, Mayuri and Padhi, Radhakant (2012) Partially integrated guidance and control of an air-dropped guided munition with explicit trajectory fixing. In: IFAC Workshop on Embedded Guidance, Navigation and Control (EGNCA), 2012, Bangalore, India.Full text not available from this repository.
An innovative partially integrated guidance and control (PIGC) technique is developed for trajectory fixing by considering six degree-of-freedom (Six-DOF) nonlinear engagement dynamics for successful interception of ground targets by guided munitions. This trajectory fixing algorithm gives closed form solution, where two different trajectories are designed in x - h and x - y planes separately using simple quadratic equations. In order to follow designed trajectories commanded pitch and yaw rates are generated in outer loop using dynamic inversion technique. In inner loop these body rates are tracked using faster dynamic inversion loop by generating the necessary control surface deflections. Simulation studies with actuator dynamics have been carried out to account for three dimensional (3D) engagement geometry to demonstrate the usefulness of PIGC technique.
|Item Type:||Conference Paper|
|Additional Information:||Copyright of this article belongs to International Federation of Automatic Control.|
|Keywords:||Partially Integrated Guidance and Control; Trajectory Fixing; Dynamic Inversion; Guided Munition|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||06 Mar 2014 11:07|
|Last Modified:||06 Mar 2014 11:07|
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