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By Agneta Balint (Ed)

ISBN-10: 9533072180

ISBN-13: 9789533072180

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P. A. Mulder Delft University of Technology The Netherlands 1. , 2007). , 1999, Fujimori et al. , 2008). Two different approaches can be distinguished in the design of these trajectory control systems. , 2001). Usually, the assumption is made that the autopilot response to heading and airspeed commands is first order in nature to simplify the design. The other design approach is to integrate the guidance and control laws into one system, in order to achieve better stability guarantees and improved performance.

However, we also have indefinite error terms due to the tracking errors and due to the command filters used in the design. As mentioned before, when no rate or magnitude limits are in effect, the difference between the input and output of the filters can be made small by selecting the bandwidth of the filters to be sufficiently larger than the bandwidth of the input signal. , 2007, Yip, 1997)). Naturally, when control or state limits are in effect, the system will in general not track the reference signal asymptotically.

28] Barrett, R. , "Modeling, Design and Testing of a Barrel-Launched Adaptive Munition," proceedings of the 4" Annual SPIE Symposium on Smart Structures and Materials, San Diego, CA, 3-6 March 1997. , Niceville, Florida, 1993. [30] Hertlein, Robert and Mark Miner, “Extended Range Guided Munition (ERGM) Safe and Arm Device and Height-of-Burst Sensor,” paper presented at the NDIA Fuse Conference, 9 April 2993, New Orleans, LA. pdf [31] Pike, J. org, Alexandria, Virginia, October, 2002. htm). , “M732A2 Proximity Fuse and M782 Multi-Option Fuse for Artillery (MOFA) Data Sheets,” published by Alliant Techsystems, Inc.

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Advances in Flight Control Systems by Agneta Balint (Ed)

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