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Browsing by Supervisor "Thomasson, P. G."

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Application of nonlinear control theory in weapon guidance and control

Brundle, D. (2001-03)

This thesis considers the application of nonlinear control theory in two subjects pertinent to weapon applications. Initially, Section 2 considers the development of a simple nonlinear autopilot for a Laser Guided Bomb ...
A combined design and trajectory optimisation algorithm for an orbiter vehicle

McGregor , Andrew. E. (Cranfield University, 1995-04)

This thesis describes the development of a computer program to optimise the design of a rocket powered orbiter vehicle, by combining a design synthesis with consideration of both the ascent and re-entry trajectories. ...
Development of a simulation tool for flight dynamics and control investigations of articulated vtol unmanned aircraft

Saghafi, F. (Cranfield University, 1996-06)

A simulation tool for flight dynamics and control investigations of three different Vertical Take Off and Landing (VTOL) unmanned aircraft configurations has been developed. A control concept has been proposed in order ...
The development of the mathematical model of an RPV and an investigation on the use of an EKF for the identification of its aerodynamic derivatives

Milonidis, E. (Cranfield University, 1987-05)

A six-degrees of freedom mathematical model of an experimental Remotely Piloted Vehicle (RPV) and the linearised longitudinal and lateral models at 30m/sec are developed. The longitudinal and lateral dynamics are analysed ...
The Development of the Mathematical Model of an RPV and an Investigation on the Use of an EKF for the Identification of its Aerodynamic Derivatives

Milonidis, E. (1987-05)

A six-degrees of freedom mathematical model of an experimental Remotely Piloted Vehicle (RPV) and the linearised longitudinal and lateral models at 30 m/sec are developed. The longitudinal and lateral dynamics are ...
Integration of global positioning and inertial reference system data inside a flight management computer

Richards, N. P. (1992-01)

A Kalman filter is used to integrate the outputs from a Global Positioning System and an Inertial Reference System inside a Flight Management Computer. To initialise the Kalman filter, account is taken of the 1RS errors ...

Browsing by Supervisor "Thomasson, P. G."

Browsing by Supervisor "Thomasson, P. G."

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