FLUID INJECTION SHOCK VECTOR CONTROL SYSTEM

Abstract

ABSTRACT A fluid injection shock vector control system (100), comprising: a plurality of fluid injectors for shockwave manipulation; a control module configured to regulate the fluid injection based on flight dynamics; a sensor array for real-time monitoring of aerodynamic conditions and vehicle performance.

Specification

Description:FIELD OF THE DISCLOSURE
[0001] This invention generally relates to a field of aerospace engineering and, in particular, to a fluid injection shock vector control system for enhancing the maneuverability of aircraft and spacecraft.
BACKGROUND

[0002] The subject matter discussed in the background section should not be assumed to be prior art merely as a result of its mention in the background section. Similarly, a problem mentioned in the background section or associated with the subject matter of the background section should not be assumed to have been previously recognized in the prior art. The subject matter in the background section merely represents different approaches, which in and of themselves may also correspond to implementations of the claimed technology.
[0003] Maneuverability and control are critical aspects of aircraft and spacecraft performance. Traditional methods of control, such as aerodynamic surfaces (e.g., ailerons, rudders, and elevators), have limitations in their ability to provide , Claims:1. A fluid injection shock vector control system (100), comprising:
a plurality of fluid injectors for shockwave manipulation;
a control module configured to regulate the fluid injection based on flight dynamics;
a sensor array for real-time monitoring of aerodynamic conditions and vehicle performance.

2. The system (100) as claimed in claim 1, wherein the fluid injectors include air jets, gas nozzles, and plasma actuators.
3. The system (100) as claimed in claim 1, wherein the control module is further configured to analyze sensor data, optimize fluid injection patterns, and ensure efficient control across varying flight conditions.
4. The system (100) as claimed in claim 1, wherein the sensor array includes pressure sensors, temperature sensors, and accelerometers.
5. The system (100) as claimed in claim 1, further comprising a user interface for real-time interaction and monitoring of system performance.
6. The system (100) as claimed in claim 1, wherein the control module utilizes advanced data analys

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