Proceedings 1992 IEEE International Conference on Robotics and Automation
DOI: 10.1109/robot.1992.220254
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Automatic guidance and control laws for helicopter obstacle avoidance

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Cited by 16 publications
(3 citation statements)
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“…A previous feasibility study has verified that, with the synthesis of a nonlinear guidance and control system in a simulation based on a B-737 model, the aircraft can achieve high-precision taxi control [16]. The study applied a form of feedback linearization [28][29][30][31] to design the Auto-Taxi Control function of Figure 5.…”
Section: Fargo Auto-taxi Functionmentioning
confidence: 99%
“…A previous feasibility study has verified that, with the synthesis of a nonlinear guidance and control system in a simulation based on a B-737 model, the aircraft can achieve high-precision taxi control [16]. The study applied a form of feedback linearization [28][29][30][31] to design the Auto-Taxi Control function of Figure 5.…”
Section: Fargo Auto-taxi Functionmentioning
confidence: 99%
“…This study applies a form of feedback linearization [7]- [9] to design the control function in the inner loop of Figure 2. Figure 3 illustrates the design concept.…”
Section: Iii21 Control Loop Structurementioning
confidence: 99%
“…Undoubtedly, some of the early pioneers in autonomous navigation for helicopters worked at NASA Ames Research Center. In the 1980's and 1990's they have published a series of papers highlighting some techniques developed for automatic Nap-Of-theEarth flights such as computer vision (Sridhar and Cheng, 1988), integration of active and passive sensors (Cheng and Sridhar, 1990), design of control strategies tested in 3D computer simulations Cheng and Lam, 1992;Zelenka et al, 1993). In the beginning, the authors developed 2D models of the environment and later on they extended the path search techniques to 3D in order to obtain a low-altitude guidance system for military helicopters.…”
Section: Introductionmentioning
confidence: 99%