Question 45-1 : A public liability insurance for your drone ? [ Success english ]

Car's 90117 right of way a pilot of a remotely piloted aircraft shall give way to power driven heavier than air aircraft airships gliders and balloons at all times

Maximum altitude 90125 1 subject to subsection 2 no pilot shall operate a remotely piloted aircraft at an altitude greater than a 400 feet 122 m agl or b 100 feet 30 m above any building or structure if the aircraft is being operated at a distance of less than 200 feet 61 m measured horizontally from the building or structure 2 a pilot may operate a remotely piloted aircraft at an altitude greater than those set out in subsection 1 if the operation is conducted in accordance with a special flight operations certificate rpas

Cars 90147 operations at or in the vicinity of an aerodrome airport or heliportno pilot shall operate a remotely piloted aircraft at or near an aerodrome that is listed in the canada flight supplement or the water aerodrome supplement in a manner that could interfere with an aircraft operating in the established traffic pattern

Division v advanced operations90169 manufacturer declaration permitted operations 1 subject to subsection 2 no pilot shall operate a remotely piloted aircraft system under this division to conduct any of the following operations unless a declaration under section 90176 has been made in respect of that model of system and the certificate of registration issued in respect of the aircraft specifies the operations for which the declaration was made a operations in controlled airspace b operations at a distance of less than 100 feet 30 m but not less than 164 feet 5 m from another person except from a crew member or other person involved in the operation measured horizontally and at any altitude or c operations at a distance of less than 164 feet 5 m from another person measured horizontally and at any altitude 2 a pilot may operate a remotely piloted aircraft system under this division to conduct the operations referred to in paragraphs 1 a and b if before april 1 2019 the model of system was determined by the minister to meet the requirements set out in appendix c criteria for a compliant small uav system design of staff instruction si no 623 001 published by the minister on november 19 2014division vi advanced operations requirements for manufacturer90176 manufacturer declaration 1 for each model of remotely piloted aircraft system that is intended to conduct any of the operations referred to in subsection 90169 1 the manufacturer shall provide the minister with a declaration in accordance with subsection 2 except in the case of a model referred to in subsection 90169 2 and that is intended to conduct any of the operations referred to in that subsection 2 the manufacturer's declaration shall a specify the manufacturer of the remotely piloted aircraft system the model of the system the maximum take off weight of the aircraft the operations referred to in subsection 90169 1 that the aircraft is intended to undertake and the category of aircraft such as a fixed wing aircraft rotary wing aircraft hybrid aircraft or lighter than air aircraft b indicate that the manufacturer i declares that it meets the documentation requirements set out in section 90178 and ii has verified that the system meets the technical requirements set out in standard 922 rpas safety assurance applicable to the operations referred to in subsection 90169 1 for which the declaration was made

Static pressure = the pressure surrounding the aircraft at its current altitude

This is an aneroid capsule that measures barometric altitude by measuring static pressure the pressure surrounding the aircraft at its current altitude

The atmospheric pressure at your current altitude presses against the piezoelectric sensor which generates a distinct and reproducible voltage proportional to that pressure consequently by knowing the local pressure as your drone ascends the atmospheric pressure will decrease or increase if you are at the top of a bridge or tower and your drone descends lower and the barometer can provide you with altitude information relative to your starting point

The aneroid capsule is used to sense absolute pressure it is used for low pressure measurement

An inertial measurement unit imu is an electronic device that measures and reports a body's specific force angular rate and sometimes the orientation of the body using a combination of accelerometers gyroscopes and sometimes magnetometers imus are typically used to maneuver aircraft an attitude and heading reference system including unmanned aerial vehicles uavs therefore you must check prior a flight that the imu is properly mounted set up and calibrated

Example 5045 50 = 50 inches for the diameter45 = 45 inches for the pitch

50 = 5 inches for the diameter45 = 45 inches for the pitch