Onboard GPS aerial photography navigation control system and control method thereof
A control system and GPS signal technology, applied in the field of navigation, can solve the problems of aircraft power consumption and endurance, increase aircraft load burden, etc., and achieve the effect of low cost and saving control links.
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Embodiment 1
[0050] Embodiment one, an airborne GPS aerial photography navigation control system, such as figure 1 shown, including:
[0051] Aviation GPS receivers, airborne computers, aviation digital cameras, display terminals;
[0052] The aviation GPS receiver is used to capture GPS signals, generate and output GPS data used to indicate the position of the system;
[0053] The on-board computer is the core of the entire on-board GPS aerial photography and navigation control system, used to receive the GPS data, and calculate and use to instruct the system (i.e. carry the The navigation information of the positional relationship between the aircraft of the system) and the route and the target point, display the navigation information on the display terminal, and perform navigation according to the navigation information, and control the aviation when the exposure conditions are met. Digital camera for exposure.
[0054] In this embodiment, multiple sets of position data of the route...
Embodiment 2
[0142] Embodiment 2, a control method of an airborne GPS aerial photography and navigation control system, comprising
[0143] Capture GPS signals, generate and output GPS data used to indicate the position of the system;
[0144] According to the location data of the route and the target point and the GPS data, calculate the navigation information for indicating the positional relationship between the system and the route and the target point;
[0145] displaying the navigation information; performing navigation according to the navigation information, and performing exposure when the exposure condition is met.
[0146] In this embodiment, the navigation information includes at least the projected distance D between the system and the target point on the horizontal plane t arg et , the angle θ between the line connecting the system and the target point and the projection of the route on the horizontal plane t arg et ;
[0147] The step of navigating according...
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