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Titlebook: Linear and Nonlinear Control of Small-Scale Unmanned Helicopters; Ioannis A. Raptis,Kimon P. Valavanis Book 2011 Springer Science+Business

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樓主: 宗派
11#
發(fā)表于 2025-3-23 13:36:12 | 只看該作者
12#
發(fā)表于 2025-3-23 16:36:58 | 只看該作者
Ioannis A. Raptis,Kimon P. Valavanisvent systems is relevant: control, communications, computer engineering, computer science, manufacturing engineering, operations research, and industrial engineering. .978-1-4419-4119-0978-0-387-68612-7
13#
發(fā)表于 2025-3-23 18:42:59 | 只看該作者
Ioannis A. Raptis,Kimon P. Valavanisvent systems is relevant: control, communications, computer engineering, computer science, manufacturing engineering, operations research, and industrial engineering. .978-1-4419-4119-0978-0-387-68612-7
14#
發(fā)表于 2025-3-24 02:00:42 | 只看該作者
Ioannis A. Raptis,Kimon P. Valavanisvent systems is relevant: control, communications, computer engineering, computer science, manufacturing engineering, operations research, and industrial engineering. .978-1-4419-4119-0978-0-387-68612-7
15#
發(fā)表于 2025-3-24 02:58:07 | 只看該作者
vent systems is relevant: control, communications, computer engineering, computer science, manufacturing engineering, operations research, and industrial engineering. .978-1-4419-4119-0978-0-387-68612-7
16#
發(fā)表于 2025-3-24 07:12:48 | 只看該作者
978-94-007-3369-5Springer Science+Business Media B.V. 2011
17#
發(fā)表于 2025-3-24 11:15:08 | 只看該作者
Linear and Nonlinear Control of Small-Scale Unmanned Helicopters978-94-007-0023-9Series ISSN 2213-8986 Series E-ISSN 2213-8994
18#
發(fā)表于 2025-3-24 17:14:38 | 只看該作者
Introduction,This Chapter presents the rationale for the book, defines the problem to be solved along with the challenges that need to be overcome, and concludes with a summary of the linear and nonlinear controller methodologies that will be detailed in subsequent Chapters.
19#
發(fā)表于 2025-3-24 22:04:40 | 只看該作者
Nonlinear Tracking Controller Design for Unmanned Helicopters,The previous Chapter presented a tracking controller of the position and heading of a helicopter based on the linearized helicopter dynamics. The adopted parametric linear model, on which the flight controller is based on, represented the quasi steady state behavior of the helicopter dynamics at hover.
20#
發(fā)表于 2025-3-24 23:42:53 | 只看該作者
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