Abstract
In a rotor propelled drone, we can control the flying momentum by the attitude of the rotorcraft. The roll, pitch, and yaw are the attitude of a rotorcraft system. For vertical climbing of the rotorcraft, the altitude comes into place.
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Reference
T.S. Ng, Rotorcrafts, in Flight Systems and Control. Springer Aerospace Technology (Springer, Singapore, 2018). https://doi.org/10.1007/978-981-10-8721-9_7
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Ng, T.S. (2021). Rotorcrafts Control Theory. In: Robotic Vehicles: Systems and Technology. Springer, Singapore. https://doi.org/10.1007/978-981-33-6687-9_16
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DOI: https://doi.org/10.1007/978-981-33-6687-9_16
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Publisher Name: Springer, Singapore
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Online ISBN: 978-981-33-6687-9
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